Items where Subject is "ENGINEERING > Structural Mechanics"

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Number of items at this level: 389.

A

Aeroelasticity Group, (1985) Aeroelastic Testing of ASLV Models for Predicting Transonic Buffet Response : Ground Studies. Project Report. National Aerospace Laboratories, Bangalore.

Aeroelasticity Group, (1985) Aeroelastic Testing of ASLV Models for Predicting Transonic Buffet Response: Model Design and fabrication. Project Report. National Aerospace Laboratories, Bangalore.

Anandan, K and Brahma, KK and Dash, PK and Raju, KN (1989) Evaluation of Fatigue and Fracture properties of Al-Li Alloys - Annual Report 1988-89. Project Report. National Aerospace Laboratories, Bangalore.

Anandan, K and Dash, PK (1991) Literature review microstructural aspects of fatigue and fracture behavior of aluminium lithium alloys. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Aravind, and Somenath, Mukharjee (2005) A Theoretical Formulation For Flutter Analysis Of A Typical Subsonic Aircraft Wing (SARAS) Using Quasi-steady Aerodynamic Theory. Project Report. National Aerospace Laboratories, Bangalore.

Aruna, HM and Guruprasad, K and Somashekar, BR (1985) Finite element modelling and analysis of a composite rudder. In: Conference on Finite Elements in Computational Mechanics, 2-6 Dec 1985, Bombay, India.

Aruna, ST and Diwakar, S and Anjana, Jain and Rajam, KS (2005) Comparative study on the effect of current density on Ni and Ni-Al nanocomposite coatings produced by electrolytic deposition. Surface Engineering, 21 (3). pp. 209-214. ISSN 0267-0844

Aruna, ST and Muniprakash, M and William Grips, VK (2013) Effect of titania particles preparation on the properties of Ni–TiO2 electrodeposited composite coatings. Journal of Applied Electrochemistry, 43 (8). pp. 805-815. ISSN 0021-891X

B

Balaraju, JN and Anandan, C and Rajam, KS (2005) Electroless deposition of ternary Ni-W-P alloys from sulphate and chloride based baths. Surface Engineering, 215 (20). pp. 215-220. ISSN 0267-0844

Balaraju, JN and Kalavati, -- and Rajam, KS (2009) Surface morphology and structure of electroless ternary NiWP deposits with various W and P contents. Journal of Alloys and Compounds, 486 . pp. 468-473. ISSN 0925-8388

Balasubramaniam, R and Ramakrishna, DS and Saraswathi , Krishna (1985) Tuning of Mechanical Vibration Absorber for seaking Helicopter. Project Report. National Aerospace Laboratories, Bangalore.

Balasubramaniam, R and Ramakrishna, DS and Vijayakumar, PS (1985) Modal analysis of a typical fighter aircraft using transient testing technique. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Balasubramaniam, R and Shankar, V and Ramakrishna, DS and Nagaraja, SV (1988) Ground Resonance studies of HS 748 (unmodified ) Aircraft. Project Report. National Aerospace Laboratories, Bangalore.

Balasubramaniam, R and Siddappa, SV and Shankar, V and Saraswathi , Krishna and Ramakrishna, DS and Shashikala, Prakash (1987) Ground Resonance Test and Response analysis of HS 748 aircraft a Preliminary report. Project Report. National Aerospace Laboratories, Bangalore.

Balasubramaniam, R and Somashekar, BR (1985) Direct digital test system for vibration studies of aircraft structures. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Balasubramaniam, R and Somashekar, BR (1994) Ground vibration studies of aerospace structures- NAL's contribution. In: Aerodynamic Testing and Structural Dynamics. Interline Publishing Private Limited, Bangalore, pp. 1-15.

Balasubramanian, TS (1988) Dynamic analysis of MiG-21 rudder (Metallic and composite). Project Report. National Aerospace Laboratories, Bangalore.

Balasubramanian, TS (1988) Dynamic strain monitoring of a EE pod during environmental tests. Project Report. National Aerospace Laboratories, Bangalore.

Balasubramanian, TS and Ramani, TS and Upadhya, AR and Elayathu, MNG (1985) Free Vibration Analysis of ASLV Aeroelastic Buffet Models. Project Report. National Aerospace Laboratories, Bangalore.

Balasubramanian, TS and Subramanian, G (1985) On the performance of a four-degree-of-freedom per node element for stepped beam analysis and higher frequency estimation. Journal of Sound and Vibration., Vol. 9 . pp. 563-567.

Balasubramanian, TS and Upadhya, AR (1985) Studies on the effects of flexibility in PSLV using aeroelastic models (A project proposal to VSSC, Trivandrum). Project Report. National Aerospace Laboratories, Bangalore.

Balasubramanian, TS and Vijaya Vittala, NG and Sudeendra, HN and Naidu, TM and Rajappa, Sashikala and Annamma Samuel, - (1985) Strain measurements on pressure vessels. Project Report. National Aerospace Laboratories, Bangalore.

Bapu Rao, MN (1985) Stress Analysis of a Missile wing subjected to Aerodynamic forces and heating. Project Report. National Aerospace Laboratories, Bangalore.

Bapu Rao, MN Three-dimensional stress problem of a finite thick plate with a through crack under tension. In: 6th International Conference on Fracture (ICF6)., 4-10 Dec 1984, New Delhi, India.

Bapu Rao, MN and Ashok Kamath, . and Kundavi Rani, . (1988) Stress Analysis of Prithvi Missil Wing Subjected to Aerodynamic Forces. Project Report. National Aerospace Laboratories, Bangalore.

Bapu Rao, MN and Dash, PK and Rani, DK (1997) Fatigue Analysis of an Aircraft Fin Lug. Project Report. National Aerospace Laboratories, Bangalore.

Bapu Rao, MN and Kamath, Ashok (1987) On the stress problem of the pebble bed heat exchanger in a hypersonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Bapu Rao, MN and Murthy, MVV (1971) On the stresses in the vicinity of an elliptic hole in a cylindrical shell under torsional loading. Nuclear Engineering and Design, 17 (3). pp. 309-321. ISSN 0029-5493

Bapu Rao, MN and Subba Rao, M and Sethuraman, Geetha and Susheela, GR (1986) Improved procedure for the determination of apparent strain. Nuclear Engineering and Design, 92 (1). pp. 27-36. ISSN 0029-5493

Bapu Rao, MN and Subramanya Sastry, SS and Dwarakanath, K and Jharia, Anoop and Rani, DK (1997) A report on the analysis of rear fitting assembly for LCA fin. Project Report. National Aerospace Laboratories, Bangalore.

Basu, Bharathibai J and Anandan, C and Rajam, KS (2004) Application of luminescent coatings for surface pressure measurements. In: International Conference on Advances in Surface Treatment: Research and Applications, ASTRA,, Nov 3-6 2003, Hyderabad, India.

Bera, Parthasarathi and Seenivasan, H and Rajam, KS and Shivakumara, C and Parida, SK (2013) Characterization and microhardness of Co-W coatings electrodeposited at different pH using gluconate bath: A comparative study. Surface and Interface Analysis, 45 (6). pp. 1026-1036.

Bhandari, SK (1974) General criterion of fracture of cracked plates. International Journal of Fracture, 10 . pp. 276-278. ISSN 0376-9429

Bhashyam, GR and Prathap, Gangan (1980) Galerkin finite element method for non-linear beam vibrations. Journal of Sound and Vibration, 72 (2). pp. 191-203. ISSN 0022-460X

Bhashyam, GR and Prathap, Gangan (1979) Galerkin finite element method for non-linear beam vibrations. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Bhaumik, SK and Raja, S and Rajagopal, P (1994) Active flutter suppression of a cantilever plate at supersonic speeds. In: Aerodynamic Testing and Structural Dynamics. Interline Publishing Private Limited, Bangalore, pp. 1-16. ISBN 81-7296-040-9

Brahma, KK (1990) Corrosion fatigue crack propagation in aluminium lithium alloys under spectrum loading. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Brahma, KK (1990) Load cell calibration of axial load fatigue testing machine. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Brahma, KK (1996) Seismic Qualification Testing of 300 AH RPC / H C P LM Cells on Steel Stand. Technical Report. National Aerospace Laboratories, Bangalore, India.

Brahma, KK (1999) Seismic Qualification Testing of Soft Starter Panel. Technical Report. National Aerospace Laboratories, Bangalore, India.

Brahma, KK (2001) Seismic qualification of Pneumatically Operated Directional Ball Valve Assembly and Fire Alaram Panel. Technical Report. National Aerospace Laboratories, Bangalore, India.

C

Chandra, R (1976) Large deflection vibration of cross-ply laminated plates with certain edge conditions. Journal of Sound and Vibration, 47 (4). pp. 509-514. ISSN 0022-460X

Chandra, R (1975) Postbuckling analysis of crossply laminated plates. AIAA Journal, 13 . pp. 1388-1389. ISSN 0001-1452

Chandra, R (1971) A note on orthotropic annular circular plate of uniform stress (Thickness function corresponding to constant velocity loading condition for orthotropic annular circular plate with uniform stress). Journal of the Aeronautical Society of India, 23 (3). pp. 167-168.

Chandra, R and Sunder, R Fatigue crack growth in patched plates under constant amplitude and flight simulation loadings. In: 6th International Conference on Fracture (ICF6)., 4-10 Dec 1984, New Delhi.

Chandra, Ramesh and Murthy, MVV and Ramamurthy, TS and Rao, AK (1985) Analytical estimation of stress intensity factors in patched cracked plates. Engineering Fracture Mechanics, 21 (1). pp. 479-494. ISSN 0013-7944

Chandra, Ramesh and Raju, Basava B (1970) Stresses around a circular hole in a shallow conical shell with torsional loading. International Journal of Solids and Structures, 6 (10). pp. 1389-1401.

Chandra, S (1999) Feature description structures for finite element modelling. In: International Conf. on Civil and Structural Engineering, 7th, and International Conf. on the Applications of AI to Civil and Structural Engineering, 13-15 Sept 1999, Oxford, UK.

Chandra, S (1998) Information extraction and qualitative descriptions from13; dynamic simulation data. Computers and Structures, 69 . pp. 757-766.

Chandra, S (1997) A tutorial and diagnostic tool for chaotic oscillators and time series13;. Computers and Graphics, 21 (2). pp. 253-262.

Chandra, Satish (2007) Market Forecasts and Cost Economics Structures For the Management of Civil Aircraft Operations in India. In: Symposium on Aircraft Design, 14th June 2007, Bangalore, India.

Chandra, Satish and Prathap, Gangan (1989) A field-consistent formulation for the eight-noded solid finite element. Computers and Structures, 33 (2). pp. 345-355. ISSN 0045-7949

Chandrasekhar, M and Sunitha, DV and Dhananjaya, N and Nagabhushana, H and Sharma, SC and Nagabhushana, BM and Shivakumara, C and Chakradhar, RPS (2012) Structural and phase dependent thermo and photoluminescent properties of Dy(OH)(3) and Dy2O3 nanorods. Materials Research Bulletin, 47 (8). pp. 2085-2094. ISSN 0025-5408

Chattopadhya, L (2003) Analytical determination of stress intensity factor for plate bending problems. International Journal of Computational Engineering Sciences., 4 (1). pp. 109-119. ISSN 1465-8763

Chattopadhyay, Lalitha (2005) Analytical solution for an orthotropic elastic plate containing cracks13;. International Journal of Fracture, 134 (3-4). pp. 305-317.

Chattopadhyay, Lalitha (2007) Analytical solution for bending stress intensity factor in an orthotropic elastic plate containing a crack and subjected to concentrated moments. Archive of Applied Mechanics, 77 (1). pp. 49-62. ISSN 0939-1533

Chattopadhyay, Lalitha and Jain, PK (2012) Buckling load and post-buckling solution for mode shape of delaminated beam. International Journal of Engineering and Applied Sciences, 4 (2). pp. 59-66.

Chopra, I and Durvasula, S (1971) Natural frequencies and modes of tapered skew plates. International Journal of Mechanical Sciences, 13 . pp. 935-944. ISSN 0020-7403

Chowdhury, P and Kulkarni, PD and Krishnan, M and Barshilia, Harish C and Sagdeo, A and Rai, SK and Lodha, GS and Sridhara Rao, DV (2012) Effect of coherent to incoherent structural transition on magnetic anisotropy in Co/Pt multilayers. Journal of Applied Physics, 112 (2). 023912-1-023912-8. ISSN 0021-8979

D

Dash, PK and Brahma, KK (1991) Random load sequence for full scale fatigue test of MiG-21M airframe. Project Report. National Aerospace Laboratories, Bangalore.

Dash, PK and Iyengar, RN (1982) Analysis of Randomly Time Varying Systems By Gaussian Closure Technique. Journal of Sound and Vibration, 83 (2). pp. 241-251. ISSN 0022-460X

Dayananda, GN and Shankaranarayan, S (1991) Air circulation unit for the 3m Dia x 7m length autoclave -A computer aided design approach. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Devi, Bharathi B (1977) Maximization of system reliability by accelerated random search algorithm. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Dutta, Soma and Raja, S and Rajappa, S and Medar, MH Modelling and Analysis of MEMS Thermal Actuator. Project Report. National Aerospace Laboratories, Bangalore, India.

F

Farook, MA and Gopalan, R and Subba Rao, M and Ramanaiah, B and Prabhakaran Nair, O and Suseela, GR and Ramachandra, HV (1996) Structural static testing of LCA rudder. Project Report. National Aerospace Laboratories, Bangalore.

G

Ghoshal, S and Sunder, R (1989) Parametric analysis of fatigue under random loading. Technical Report. Structural Sciences Division, Bangalore, India.

Gopalan, R and Farook, MA (1994) Static testing of LCA co-cured fin (Preliminary report). Project Report. National Aerospace Laboratories, Bangalore.

Gopalan, R and Ramanaiah, B and Farook, MA and Ramachandra, HV and Sudheendra, HN and Suseela, GR (1990) Static testing of bridge deck plate prototypes. Project Report. National Aerospace Laboratories, Bangalore.

Gopalan, R and Ramesh Chandra, . (1987) Static Testing of Metallic Rudder of a Military Aircraft. Project Report. National Aerospace Laboratories, Bangalore.

Guruprasad, K and Aruna, HM (1985) Application of ASKA to a multirib box structure. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Guruprasad, K and Subba Rao, M and Chandra, Ramesh (1988) Finite element analysis of composite rudder for DO 228 Aircraft 13; 13;. In: Composite Materials and Structures, 6-9 Jan 1988, Madras, India.

H

Himanshu, L Dave and Raja, S and Vijaya Kumar, MP (2009) Design and Development of Active Fasteners with PZT Stack Actuators for Vibration Control Applications. Project Report. NAL, Bangalore.

Hussainy, SA and Hasseem, Mohamed H and Bhagawan, GK (1970) Stress distribution in the vicinity of slender notches having arbitrary shapes. Experimental Mechanics, 10 (1). pp. 46-48.

I

Ismail, Shaik and Chetty, Shyam and Raol, JR (1989) Longitudinal equivalent systems for augmented aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Iyer, RV and Sudhakar, A and Vijayan, Kalyani (2006) Decomposition behavior of kevlar 49 fibers: Part II. At T values lt; Td. High Performance Polymers, 18 . pp. 495-517.

J

Jafarali, P and Chattopadhyay, Lalitha and Prathap, Gangan and Rajendran, S (2004) Error analysis of a hybrid beam element with Timoshenko stiffness and classical mass. International Journal of Computational Engineering Science, 5 (3). pp. 495-508.

Jain, Anjana and Vijayan, Kalyani (2004) Forbidden reflections from the aramid PPTA-A novel correlation13; with stacking faults. Bulletin of Material Science, 27 (1). pp. 47-50.

Jain, Saransh and Viswamurthy , SR and Gupta, Nitesh (2012) Debond Detection and Load Estimation Using Fiber Bragg Grating Sensors on a Composite Test Box – Part II (Algorithm Development). In: International Conference on Smart Materials Structures and Systems, 4-7 January 2012, Indian Institute of Science, Bangalore.

Janardhanam, S and Dutta, Soma and Rajappa, S and Sundararajan, D and Raja, S (2004) Characterization of piezoelectric stack actuators for structural control applications. In: 3rd International Conference on Theoretical, Applied, Computational and Experimental Mechanics – ICTACEM 2004 , December 2004, IIT, Kharagpur, India.

Jarali, Chetan S and Raja, S and Upadhya, AR (2010) Constitutive modeling of SMA SMP multifunctional high performance smart adaptive shape memory composite. Smart Materials and Structures, 19 (10). ISSN 0964-1726

Jayanthi, BG (1989) Floating point hardware for the Flosolver. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Jayanthi, BG (1989) Multiactuator controller for full-scale fatigue test. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Jayaraman, Chatterjee A and Ramaseshan, S and Singh, AK (1972) Pressure-induced electronic and structural transformation in some rare earth monochalcogenides. Acta Crystallographica, A28 . S243-S243.

Jayasurya, M and Viswanathan, KS and Subba Rao, M (1990) Fabrication of GFRP bridge deck plate using soft tools. Project Report. National Aerospace Laboratories, Bangalore.

Joshi, A (1988) Free vibration analysis of HS0748 L Theoretical study and comparison with test results. Project Report. National Aerospace Laboratories, Bangalore.

Joshi, A and Madhusudan, BS (1988) Free Vibration analysis of Rotodome - pylon assembly. Project Report. National Aerospace Laboratories, Bangalore.

Joshi, A and Madhusudan, BS (1989) Free Vibration, Flutter and Gust Response Analysis of HS-748 Modified for AEW Role. Project Report. National Aerospace Laboratories, Bangalore.

Joshi, A and Madhusudhan, BS (1988) Free vibration analysis of Free vibration analysis of HS-748 integrated with pylone and deck plate. Project Report. National Aerospace Laboratories, Bangalore.

Joshi, A and Madhusudhan, S (1991) Sensitivity of free vibration charecteristices of cantilever plates to geometric parameters. Journal of Sound and Vibration, 145 (3). pp. 489-494.

Joshi, A and Rajagopal, P (1985) Theoretical studies of wing divergence. Project Report. National Aerospace Laboratories, Bangalore.

Joshi, A and Ramamurthy, MR (1988) Aeroelastic testing of PSLV models. Project Report. National Aerospace Laboratories, Bangalore.

Joshi, A and Somashekar, BR (1988) Effect of initial curvature on the panel flutter. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Joshi, A and Somashekar, BR (1986) Effect of static inplane loads and boundary conditions on the flutter of flat rectangular panels. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Joshi, A and Somashekar, BR (1986) Effect of static inplane loads and boundary conditions on the flutter of flat rectangular panels. Journal of Aeronautical Society of India, 38 . pp. 105-112.

Joshi, A and Suryanarayan, S (1989) Unified analytical solution for various boundary conditions for the coupled flexural-torsional vibration of beams subjected to axial loads and end moments. Journal of Sound and Vibration, 129 . pp. 313-326. ISSN 0022-460X

Joshi, A and Upadhya, AR (1987) Modal couping effects in the free vibration of elastically interconnected beams. Journal of Sound and Vibration, 117 (1). pp. 115-130. ISSN 0022-460X

Joshi, A and Upadhya, AR (1986) Transonic Buffet Testing of the PSLV Models - II: Modified Design & analysis. Project Report. National Aerospace Laboratories, Bangalore.

Joshi, A and Upadhya, AR (1986) Vibration of beams on intermediate elastic supports. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Joshi, A and Upadhya, AR and Balasubramanian, TS (1985) Transonic buffet testing of the PSLV models - I. Project Report. National Aerospace Laboratories, Bangalore.

Joshi, SC and Subba Rao, M and Murthy, MVV (1990) FEM analysis of GFRP single cell test beam and modified GFRP bridge deck. Project Report. National Aerospace Laboratories, Bangalore.

K

Kamalakannan, GM and Subba Rao, M and Chandra, K and Abhilash, P (2008) Advanced hot bonding system for repair of Aerospace Structures. In: Proceedings of the INCCOM-7, Dec. 4-5, 2008, Bangalore, India.

Kamath, GM and Kumar, Senthil P and Shivaprasad, MV (2002) Vibration control studies using an impedance method. In: Conference on Smart Materials, Structures, and Systems, 12-14 Dec 2002, Bangalore, India.

Kamath, GM and Sundaram, Ramesh and Gupta, Nitesh and Rao, Subba M (2010) Damage studies in composite structures for structural health monitoring using strain sensors. Structural Health Monitoring, 9 (6). pp. 497-512. ISSN 14759217

Kariappa, - and Somashekar, BR (1965) Application of matrix displacement methods in the study of panel flutter. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Kariappa, - and Somashekar, BR and Shah, CG (1970) Discrete element approach to flutter of skew panels with13; in-plane forces under yawed supersonic flow. AIAA Journal, 8 (11). pp. 2017-2022.

Kariappa, V and Somashekar, BR (1970) Flutter of skew panels by the matrix displacement approach. The Aeronautical Journal of the Royal Aeronautical Society, 74 (716). pp. 672-675.

Karthikeyan, K and Ramachandra, S and Vizhian, Paul S and Chandra, Satish (2011) Signal processing, wavelets and high-speed image interpretation of bird impact. Defence Science Journal, 61 (1). pp. 62-71. ISSN 0011-748X

Kaul, Anup and Sunder, R and Venkatesh, CS (1989) 64 Channel Z80 microprocessor based strain gauge data13; acquisition system. Technical Report. National Aeronautical Laboratory, Bangalore, India.

KavithaMol , S and Stanley, C. Salem (2011) Parametric Studies on Bird Impact Behavior of Aircraft Leading Edges. Masters thesis, National Aerospace Laboratories, Bangalore.

Kidambi, R (2009) Viscous oscillations in a circular cylinder with an elastic cover on the free surface. Journal of Engineering Mathematics, 64 (3). pp. 269-284.

Kumar, AS and Kumar, BR and Datta, GL and Ranganath, VR (2010) Effect of microstructure and grain size on the fracture toughness of a micro-alloyed steel. Materials Science and Engineering A, 527 (4-5). pp. 954-960. ISSN 0921-5093

Kumar, D Nagendra and Raja, S and Yadav, D (2005) Active vibration control of composite plate with partially13; debonded piezoelectric actuators. In: International Conference on Smart Materials Structures and Systems, 28-30 Jul 2005, Bangalore, India.

Kumar, GV and Rao, KM and Kumar, JS and Raja, S (2011) Selective modal space control approach for smart composite cylindrical shell structure. ARPN Journal of Engineering and Applied Sciences, 6 (3). pp. 67-74. ISSN 1819-6608

L

Lakshminarayana, HV (1984) Study of interlaminar fracture in unidirectional composite materials. In: Analysis of Structures - A Commemorative volume published on the occasion of the 60th Anniversary of Dr. S.R.Valluri, Dec 1984, NAL, Bangalore, India.

Lakshminarayana, HV and Kailash, K (1989) A shear deformable curved shell element of quadrilateral shape. Computers and Structures, 33 (4). pp. 987-1001.

Lakshminarayana, HV and Murthy, MVV and Srinath, LS (1982) On an analytical-numerical procedure for the analysis of cylindrical shells with arbitrarily oriented cracks. International Journal of Fracture, 19 . pp. 257-275. ISSN 0376-9429

Lakshminarayana, HV and Murthy, MVV and Srinath, LS (1981) On finite element model for the analysis of through cracks in laminated anisotropic cylindrical shells. Engineering Fracture Mechanics, 14 (4). pp. 697-712. ISSN 0013-7944

Lakshminarayana, HV and Ramani, TS (1988) On improving the performance of a shear-flexible triangular laminated composite plate finite element. In: Proceedings of the International Conference on Composite materials and structures, 6-9 Jan 1988, Madras, India.

Lakshminarayana, HV and Ramesh Babu, C (1985) Finite Element Applications in Mechanics of Composites. In: Finite Elements in Computational Mechanics., 2-6 Dec 1985, Bombay; India.

Lakshminarayana, HV and Viswanath, S (1976) Influence of material orthotropy on the state of stress around a circular hole in a cylindrical shell. In: ASME 1976, 5-10 Dec 1976, New York, USA.

M

Madhava, MR and Sudheendra, HN (1985) Acoustic Emission Monitoring of Ammonia Transfer Main Weld Joints. Project Report. National Aerospace Laboratories, Bangalore.

Madhava, MR and Sudheendra, HN and Sridhara, S and Ramachandra, HV (1988) NON- Destructive Evaluation of Mig 21 composite Rudder. Project Report. National Aerospace Laboratories, Bangalore.

Madhava, MR and Sudheendra, HN and Sridhara, S and Ramachandra, HV (1989) Non Destructive Evaluation of MiG-21 Compsoite Rudder Part II - APT Section Adhesive bond qulality Evaluation. Project Report. National Aerospace Laboratories, Bangalore.

Madhava, MR and Upadhya, AR and Jayasurya, M (1985) Tests on Redux Bonded Sandwich Specimens. Project Report. National Aerospace Laboratories, Bangalore.

Madhusudhan, BS (1994) Buckling of simply supported laminated composite and sandwich panels including the effect of stringer stiffeners. Technical Report. National Aerospace Laboratories, Bangalore,India.

Madhusudhan, S (1994) Buckling of simply supported laminated composite and sandwich panels including the effect of stringer stiffeners. Technical Report. National Aerospace Laboratories, Bangalore,India.

Malwadkar, S and Bera, Parthasarathi and Hegde, MS and Satyanarayana, CVV (2012) Preferential oxidation of CO on Ni/CeO2 catalysts in the presence of excess H-2 and CO2. Reac Kinet Mech Cat, 107 . pp. 405-419.

Mani, A and Pai, BC and Vijayan, Kalyani (1986) Comparison of the graphitizabilities of heat-treated coal tar and its mesophase pitches. Journal of Materials Science Letters, 5 (5). pp. 506-508. ISSN 0261-8028

Manjunatha, C.M. and Ramesh , Bojja and Jagannathan, N and Kinloch, A.J. and Taylor, A.C. (2013) Enhanced fatigue behavior of a glass fiber reinforced hybrid particles modified epoxy nanocomposite under WISPERX spectrum load sequence. International Journal of Fatigue, 54 . pp. 25-31. ISSN 0142-1123

Manjunatha, CM and Parida, BK (2003) A model for predicting the overload effects on fatigue crack growth behavior. In: 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 7-10 Apr 2003.

Manjunatha, CM and Ramesh , Bojja and Jagannathan, N Fatigue Behavior of a Nanocomposite Under a Fighter Aircraft Spectrum Load Sequence. Journal of Nano Research, 24 . pp. 58-66. ISSN 1661-9897

Manjuprasad, M and Sathish, B S and Viswanath, S (2007) Dynamic aeroelastic subsonic discrete gust response analysis of lifting surfaces in time domain using Newark's method. Technical Report. National Aerospace Laboratories, Bangalore, India.

Manjuprasad, M and Manohar, CS (2006) Stochastic finite element reliability analysis of plates/shells under dynamic excitations with adaptive mesh refinements. In: International Conference on Trends in Product Life Cycle-Modeling, Simulation and Synthesis (PLMSS-06), 18-20 Dec 2006, Bangalore, India.

Marimuthu, V and Raja, S and Viswanath, S and Rajesh, C (2004) Finite element formulation and analysis of laminated piezoelectric sandwich shells. Technical Report. National Aerospace Laboratories, Bangalore, India.

Marur, SR and Prathap, Gangan (2000) Consistency and correctness evaluation of shear deformable13; anisoparametric formulations. International Journal of Solids and Structures, 37 (5). pp. 701-713.

Mary, Shini Mole and Naganarayana, BP and Pratap, G (1994) FEM analysis of LTA-7 horizontal tail. Project Report. National Aerospace Laboratories, Bangalore.

Mohan, Kumar M (2010) Residual strength evaluation of a transport aircraft fuselage stiffened panel. In: Proceedings of International Conference on Frontiers in Mechanical Engineering , , 20-22 May 2010, NITK,Surathkal, Mangalore, Karnataka, INDIA.

Mohan, Kumar M and Jagannathan, N and Jeeva, Peter M and Ravi, Kumar S (2010) Hygrothermal effects on the mechanical properties of glass fibre-epoxy composite material. In: Proceedings of Second International Conference on Polymer Processing and Characterization , 15-17 Jan 2010, Kottayam, Kerala.

Mohan, Kumar M and Rajesh, S and Yogesh, H and Yeshaswini, BR (2013) Study on the effect of stress concentration on cutout orientation of plates with various cutouts and bluntness. International Journal of Modern Engineering Research, 3 (3). pp. 1295-1303. ISSN 2249-6645

Mukherjee, Somenath and Deepa, N and Avinash, R and Manjuprasad, M and Viswanath, S (2007) Analytical investigation of supersonic panel flutter under thermal environment with arbitrary flow direction. Technical Report. National Aerospace Laboratories, Bangalore, India.

Mukherjee, Somenath and Manju, S (2011) An improved parametric formulation for the variationally correct distortion immune three-noded bar element. Structural Engineering and Mechanics . ISSN 1225-4568

Mukherjee, Somenath and Manju, S (2011) An improved parametric formulation for the variationlly correct distortion immune three-noded bar element. Structural Engineering and Mechanics, 38 (3). 000-000.

Mukherjee, Somenath and Manjuprasad, M and Avinash, R and Sakravarthini, Deepa S (2007) Finite element studies on supersonic panel flutter under high thermal environment with arbitrary flow direction. Technical Report. National Aerospace Laboratories, Bangalore, India.

Mukherjee, Somenath and Prakash, B M Shashi and Alok, P Burgul and Viswanathan, S (2007) A method for dynamic characterization and response predication using ground vibration test(GVT) data for unknown structure. Technical Report. National Aerospace Laboratories, Bangalore, India.

Mukherjee, Somenath and Prathap, Gangan (2001) Analysis of shear locking in Timoshenko beam elements using the function space approach. Communications in Numerical Methods in Engineering, 17 (6). pp. 385-393.

Mukherjee, Somenath and Prathap, Gangan (2009) Lectures in FEA (Fundamentals) Lecture 1- Finite Element Analysis using Simple Elements. [Lectures/Presentation]

Mukherjee, Somenath and Prathap, Gangan (2009) Lectures in FEA (Fundamentals) Lecture 2 - Variational Principles in Computational Solid Mechanics. [Lectures/Presentation]

Mukherjee, Somenath and Prathap, Gangan (2009) Lectures in FEA (Fundamentals) Lecture 3 - The best-fit paradigm of FEA: Shadows of the exact. [Lectures/Presentation]

Mukherjee, Somenath and Prathap, Gangan (2009) Lectures in FEA (Fundamentals) Lecture 4 - Special topics of FEA. [Lectures/Presentation]

Murthy, AV and Rama Krishna, K and James, Deepa (1994) Static analysis of LTA engine mount. Project Report. National Aerospace Laboratories, Bangalore.

Murthy, HS (1984) Analysis of unsteady pressure measurements on a supercritical airfoil with a harmonically oscillating trailing edge flap at subsonic and transonic speeds. In: Forschungsbericht - Deutsche Forschungs- und Versuchsanstalt fur Luft-, 1984, Germany.

Murthy, MVV and Prathap, Gangan (1996) Shear force predictions from RBF corrected QUAD4 elements. Communications in Numerical Methods in Engineering, 12 (2). pp. 135-140. ISSN 1552-485X

Murthy, MVV and Raju, KN and Viswanath, S (1981) On the bending stress distribution at the tip of a stationary crack from Reissner's theory. International Journal of Fracture, 17 . pp. 537-539. ISSN 0376-9429

Murthy, MVV and Rao, KP and Rao, AK (1974) On the stress problem of large elliptical cutouts and cracks in circular cylindrical shells. International Journal of Solids and Structures, 10 . pp. 1243-1269. ISSN 0020-7683

Murthy, SS and Gallagher, RH (1986) Triangular thin-shell finite element based on discrete kirchhoff theory. Computer Methods in Applied Mechanics and Engineering, 54 (2). pp. 197-222.

Murthy, Sridhara S (2007) Elasto-Plastic Stress Analysis of a High Stress Region Of Saras Aircraft Wing. In: Symposium on Aircraft Design, 14th June 2007, Bangalore, India.

Murthy, Sridhara S (1984) Triangular thin shell finite element for laminated general shells. In: Analysis of Structures - A Commemorative volume published on the occasion of the 60th Anniversary of Dr. S.R.Valluri, Dec 1984, NAL, Bangalore, India.

Murthy, Sridhara S and Gallargher, RH (1985) A triangular thin shell element based on discrete Kirchhoff theory - Some patch test solution results. In: Conference on Finite elements in computational mechanics, 2-6 Dec 1985, Bombay, India.

N

Naganarayana, BP and Prasad, Vishnu T and Prathap, Gangan (1989) Implementation of Three-Noded Shear-Flexible Field-Consistent Isotropic/Anisotropic/Layered-Composite general curved beam with varying sectional rigidities in SAP-IV. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Naganarayana, BP and Prathap, Gangan (1988) Consistency aspects of out-of plane bending, torsion and shear in a quadratic curved beam element. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Naganarayana, BP and Prathap, Gangan (1990) Consistency aspects of out-of-plane bending, torsion and shear in a quadratic curved beam element. International Journal for Numerical Methods in Engineering, 30 . pp. 431-443.

Naganarayana, BP and Prathap, Gangan (1988) Consistent force resultant distributions in a quadratic Cquot; beam element with varying sectional properties. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Naganarayana, BP and Prathap, Gangan (1989) Displacement and stress predictions from field- and line-consistent versions of the eight-node Mindlin plate element. Computers and Structures, 33 (4). pp. 1095-1106. ISSN 0045-7949

Naganarayana, BP and Prathap, Gangan (1992) Expert systems and finite element structural analysis - a review. Sadhana, 17 (2). pp. 275-298.

Naganarayana, BP and Prathap, Gangan (1989) Force and moment corrections for the warped four-node quadrilateral plane shell element. Computers and Structures, 33 (4). pp. 1107-1115. ISSN 0045-7949

Naganarayana, BP and Prathap, Gangan and Ningaiah, - and Geetha, B and Manju, S (1993) FEM design and analysis of HAL - Autoclave. Project Report. National Aerospace Laboratories, Bangalore.

Naganarayana, BP and Virupaksha, SA and Prathap, Gangan (1993) Design and development of an expert advisor for general purpose finite element modeling of 2-dimensional structures. Technical Report. National Aerospace Laboratories, Bangalore, India.

Naik, N K and Veera Sesha Kumar, C Ballistic impact behavior of foam core sandwich structures: Formulation. In: International Conference on Composites - Current and Future Trends, Indian Institute of Science.

Naik, Viveka and Sundeendra, HN and Madhava, MR and Manoharan, LC (1986) Development of an acoustic emission analyzer. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Nandakumar, T and Manjuprasad, M and Vishnuram, BG (2006) Nonlinear pushover analysis of a framed structure with base isolation system. In: National Conference on Frontline Aeras of Engineering (NCFACE-2006), 28-29 Apr 2006, Coimbatore, Tamil Nadu, India.

Narayana, HVL and Rajagopal, P and Namani, TS and Ramamurthy, MR (1988) Vibration and flutter analysis of composite wing panels. In: Composite materials and structures; Proceedings of the International Conference, 6-9 Jan. 1988, Madras, India.

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Panda, PK and Sahoo, B and Raja, S and Vijayakumar, MP and Shankar, V (2012) Electromechanical and dynamic characterization of in-house-fabricated amplified piezo actuator. Smart Materials Research, 2012 .

Pandya , KS and Veera Sesha Kumar, C and Nair, NS and Patil, PS and Naik, NK (2014) Analytical and experimental studies on ballistic impact behavior of 2D woven fabric composites. International Journal of Damage Mechanics . pp. 1-41.

Pany, Chitaranjan and Parthan, S and Mukherjee, S (2002) Vibration analysis of multi-supported curved panel using the periodic structure approach. International Journal of Mechanical Sciences, 44 (2). pp. 269-285.

Parida, BK and Brahma, KK (1994) Residual Life Assessment of Ageing Aircraft - A Perspective. Technical Report. National Aerospace Laboratories, Bangalore, India.

Pavan Kumar, DVTG and Sathiya Naarayan, S and Kalyana Sundaram, S and Satish, Chandra (2012) Further numerical and experimental failure studies on single and multi-row riveted lap joints. Engineering Failure Analysis, 20 . pp. 9-24. ISSN 1350-6307

Pavani , Udatha and Veera Sesha Kumar, C and Nithin, Nair and Naik, NK (2012) High Velocity Impact Performance of three-dimensional woven composites. The Journal of Strain Analysis for Engineering Design, 47 (7). pp. 419-431.

Poojary, Aithu and Rajagopalan, SR (1986) Use of phase-locked loop for generation of reference square waves for higher harmonic AC polarography. Indian Journal of Technology, 24 (8). pp. 501-504.

Prabhu, ALM and Prakash, PJ and Thomas, SG and Vital, R and Sunder, R (1989) Subroutine package for menu driven data input. Technical Report. National Aeronautical laboratory, Bangalore, India.

Prakash, Raghu V and Mitchenko, EI (1994) A Study of Naturally Initiating Notch Root Fatigue Cracks Under Spectrum Loading. Technical Report. National Aerospace Laboratories, Bangalore, India.

Prakash, Raghu V and Parida, BK (1997) Fatigue Crack Growth Properties of Aluminium- Lithium Alloy 1441. Technical Report. National Aerospace Laboratories, Bangalore, India.

Prakash, Raghu V and Sunder, R (1991) Fatigue life under random load history derived from exceedance curves using different algorithms. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prakash, Raghu V and Sunder, R and Mitchenko, EI (1996) Study of naturally initiating notch root fatigue cracks under spectrum loading. In: Proceedings of the 3rd Symposium on Advances in Fatigue Lifetime Predictive Techniques, 16-17 May 1994, Montreal, Canada.

Prakash, Raghu V and Sunder, R and Venkatesh, CS (1990) Cyclic stress-strain curve at a semi-circular notch. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prakash, Raghu V and Venkataswamy, MA and Krishnan, RV and Raju, KN (1997) Crack front mapping technique to understand behavior of fatigue cracks in lug joints. Technical Report. National Aerospace Laboratories, Bangalore, India.

Prakash, Shashikala and Balasubramaniam, R and Praseetha, KK (2002) Simulation studies for multichannel active vibration control. In: Conference on Smart Materials, Structures, and Systems, 12-14 Dec 2002, Bangalore, India.

Prathap, Gangan (1985) Additional stiffness parameter measure of error of the second kind in the finite element method. International Journal for Numerical Methods in Engineering, 21 (6). pp. 1001-1012.

Prathap, Gangan (1996) Barlow points and gauss points and the aliasing and best fit paradigms. Computers amp; structures, 58 (2). pp. 321-325.

Prathap, Gangan (1985) Co Continuous four-noded cylindrical shell element. Computers and Structures, 21 (5). pp. 995-999.

Prathap, Gangan (1985) A Co continuous four-noded cylindrical shell element. Computers and Structures, 21 (5). pp. 995-999. ISSN 0045-7949

Prathap, Gangan (1985) Curved beam/deep arch/finite ring element revisited. International Journal for Numerical Methods in Engineering, 21 (3). pp. 389-407.

Prathap, Gangan (1984) Field consistency and the finite element analysis of multi-field structural problems. In: Analysis of Structures - A Commemorative volume published on the occasion of the 60th Anniversary of Dr. S.R. Valluri, Dec 1984, NAL, Bangalore, India.

Prathap, Gangan (1986) Field-consistency - Toward a science of constrained multi-strain-field finite element formulations. Sadhana - Academy Proceedings in Engineering Sciences, 9 (4). pp. 319-343.

Prathap, Gangan (1997) Field-consistency approach to plate elements. Structural Engineering and Mechanics, 5 (6). pp. 853-865. ISSN 1225-4568

Prathap, Gangan (1986) Field-consistency: Toward a science of constrained multi-strain-field finite element formulations. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan (1979) On the Berger approximation - A critical re-examination. Journal of Sound and Vibration, 66 . pp. 149-154.

Prathap, Gangan (1985) Poor bending response of the four-node plane stress quadrilateral. International Journal for Numerical Methods in Engineering, 21 (5). pp. 825-835.

Prathap, Gangan (1985) Simple plate/shell triangle. International Journal for Numerical Methods in Engineering, 21 (6). pp. 1149-1156. ISSN 0029-5981

Prathap, Gangan (1983) Two Frequency spectra of timoshenko beams. Journal of Sound and Vibration, 90 (3). pp. 443-446. ISSN 0022-460X

Prathap, Gangan (1993) Variational basis for Barlow points. Computers and Structures, 49 (2). pp. 381-383. ISSN 0045-7949

Prathap, Gangan (1996) Vibrations of laminated beams using higher-order theory. Advanced Composite Materials, 6 (1). pp. 33-50. ISSN 0924-3046

Prathap, Gangan (1985) An additional stiffness parameter measure of error of the second kind in the finite element method. International Journal for Numerical Methods in Engineering., 21 . pp. 1001-1012.

Prathap, Gangan (1984) An optimally constrained 4 node quadrilateral thin plate bending element. Computers and Structures, 18 (5). pp. 789-794. ISSN 0045-7949

Prathap, Gangan (1999) A priori error estimation of finite element models from first principles. Sadhana, 24 . pp. 199-214. ISSN 0256-2499

Prathap, Gangan (1985) A simple plate/shell triangle. In: International Journal for Numerical Methods in Engineering, June 1985, United Kingdom.

Prathap, Gangan (1988) The variational basis for the least-squares field- redistribution of strainFunctions in the finite element formulation of constrained media elasticity. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Bhashyam, GR (1982) Reduced integration and the shear-flexible beam element. International Journal for Numerical Methods in Engineering, 18 . pp. 195-210. ISSN 0029-5981

Prathap, Gangan and Chandra, S (1987) Field consistency and flexure of the eight noded solid element. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Prathap, Gangan and Chandra, Satish and Srinidhi, Neela and Naganarayana, BP (1989) General purpose finite element shell in 'C'. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Manju, S and Senthilkumar, V (2007) Unsymmetric finite element formulation and variational incorrectness. Structural Engineering Mechanics, 26 (1). pp. 31-42.

Prathap, Gangan and Naganarayana, BP (1990) A 3-D finite element package with expert system adaptive mesh control: Annual progress report. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Naganarayana, BP (1991) A 3-D finite element package with expert system and adaptive mesh control : User's demonstration manuals. Technical Report. National Aerospace Laboratories, Bangalore, India.

Prathap, Gangan and Naganarayana, BP (1991) A 3-D finite element package with expert system and adaptive mesh control program lists. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Naganarayana, BP (1991) A 3-D finite element package with expert system and adaptive mesh control: Concluding Report. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Naganarayana, BP (1988) Analysis of locking and stress oscillations in a general curved beam element. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Naganarayana, BP (1990) Analysis of locking and stress oscillations in a general curved beam element. International Journal for Numerical Methods in Engineering, 30 (1). pp. 177-200. ISSN 0029-5981

Prathap, Gangan and Naganarayana, BP (1988) Consistency and orthogonality requirements and accurate stress recovery from the assumed strain eight noded quadrilateral plate bending element. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Prathap, Gangan and Naganarayana, BP (1988) Field-consistency rules for a three-moded shear flexible beam element under non-uniform isoparametric mapping. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Naganarayana, BP (1988) Field-consistency rules for a three-noded shear flexible beam element under non-uniform isoparametric mapping13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Naganarayana, BP (1992) Stress oscillations and spurious load mechanisms in variationally inconsistent assumed strain formulations. International Journal for Numerical Methods in Engineering, 33 (10). pp. 2181-2197. ISSN 0029-5981

Prathap, Gangan and Naganarayana, BP and Somashekar, BR (1988) Field-consistency analysis of the isoparametric eight-noded plate bending element. Computers and Structures, 29 (5). pp. 857-873. ISSN 0045-7949

Prathap, Gangan and Naganarayana, BP and Sudhakar, B (1991) Development of general purpose finite element package for structural analysis of Isotropic, Anisotropic and Layered Composite Structures: Progress Report. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Ramesh Babu, C (1985) Accurate force evaluation with a simple bi-linear plate bending element. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Ramesh Babu, C (1987) Accurate force evaluation with a simple bi-linear, plate bending element. Computers and Structures, 25 (2). pp. 259-270. ISSN 0045-7949

Prathap, Gangan and Ramesh Babu, C (1986) Field consistent three-noded quadratic curved axisymmetric shell element. International Journal for Numerical Methods in Engineering, 23 (4). pp. 711-723.

Prathap, Gangan and Ramesh Babu, C (1986) On the fiction of the kirchhoff effective shear reactions. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Ramesh Babu, C (1986) What are the true boundary conditions on the edge of a thin plate-poisson's or kirchhoff's? Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Ramesh Babu, C and Somashekar, BR (1986) Single element test for aspect ratio sensitivity of solids - A field consistency error model. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Ramesh Babu, C and Subramanian, G (1987) Stress oscillations in plane stress modelling of flexure - A field-consistency interpretation. International Journal for Numerical Methods in Engineering, 24 (4). pp. 711-724. ISSN 0029-5981

Prathap, Gangan and Rameshbabu, C (1986) Accurate shear force evaluation with a simple bi-linear plate bending element. In: International Symposium on Composite Materials and Structures, 10-13 Jun 1986, Beijing, China.

Prathap, Gangan and Rameshbabu, C (1985) Field-Consitent strain interpolations for the quadratic shear flexible beam element. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Prathap, Gangan and Rameshbabu, C (1985) Field-consistency and violent stress oscillations in finite element method. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Rameshbabu, C (1987) Field-consistency and violent stress oscillations in the finite element method 13; 13;. International Journal for Numerical Methods in Engineering, 24 . pp. 2017-2033.

Prathap, Gangan and Rameshbabu, C (1986) Isoparametric quadratic thick curved beam element. International Journal for Numerical Methods in Engineering, 23 (9). pp. 1583-1600.

Prathap, Gangan and Rameshbabu, C (1985) A field-consistent three-noded quadratic curved axisymmetric shell element. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Rameshbabu, C (1985) An isoparametric quadratic thick curved beam element. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Rameshbabu, C (1985) An isoparametric quadratic thick curved beam element. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Senthilkumar, V and Manju, S (2006) Mesh distortion immunity of finite elements and the best-fit paradigm,. Sadhana, 31 (1). pp. 505-514.

Prathap, Gangan and Somashekar, BR (1987) Field and edge consistency synthesis of a 4-Noded quadrilateral plate bending element. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Somashekar, BR (1986) A field-consistent 8-noded laminated anisotropic plate element. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Somashekar, BR (1988) A field-consistent 8-noded laminated anisotropic plate element. In: Proceedings of the International Conference on Composite materials and structures, 6-9 Jan 1988, Madras, India.

Prathap, Gangan and Subramanian, G and Ramesh Babu, C (1985) Stress oscillations in plane stress modelling of flexure - A field- consistency interpretation. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Vinayak, RU (1996) Best-fit stress performance of a higher-order beam element13;. Communications in Numerical Methods in Engineering, 12 (4). pp. 229-234. ISSN 0748-8025

Prathap, Gangan and Vinayak, RU and Naganarayana, BP (1996) Beam elements based on a higher order theory-II - Boundary layer sensitivity and stress oscillations. Computers amp; Structures, 58 (4). pp. 791-796.

Prathap, Gangan and Viswanath, S (1983) Optimally integrated four-node quadrilateral plate bending element. International Journal for Numerical Methods in Engineering, 19 . pp. 831-840. ISSN 0029-5981

Premkumar, HB and Sunitha, DV and Nagabhushana, H and Sharma, SC and Nagabhushana, BM and Shivakumara, C and Rao, JL and Chakradhar, RPS (2012) Thermoluminescence, photoluminescence and EPR studies on Mn2+ activated yttrium aluminate (YAlO3) perovskite. Journal of Luminescence, 132 (9). pp. 2409-2415. ISSN 0022-2313

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Radhakrishna, BS and Lakshminarayana, HV (1986) Structural analysis of a Light Canard Research Aircraft using the ASKA system. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Radhakrishna, BS and Ramani, TS and Somashekar, BR (1987) Use of postprocessor femview to interactively view structural displacements. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Raghu Prasad, BK and Pavan Kumar, DVTG (2009) Fracture Behavior of Multidirectional DCB Specimen:Higher-Order Beam Theories. Journal of Engineering Mechanics , 135 (10). pp. 1119-1128.

Raja, S (2005) Modeling, simulation and implementation of smart concepts13; for structural control applications. In: lnternational Conference on Smart Materials Structures and Systems, 28-30 Jul 2005, Bangalore, India.

Raja, S and Balasubramaniam, R and Bhattacharya, Partha and Cjunjanna, G (2001) Damage modelling and prediction using smart structure concepts - A finite element analysis approach. In: ICTACEM 2001: Second International Conference on Theoretical, Applied, Computational and Experimental Mechanics, 27-30 Dec 2001, Kharagpur, India.

Raja, S and Dwarakanathan, D (2009) MAV Structures and smart Materials Applications. In: MAV Workshop- Challenges and Presferred Outcomes, 13 November 2008, National Aerospace Laboratories.

Raja, S and Rohwer, K and Rose, M (2004) Piezothermoelastic Modeling and Active Vibration Control of Laminated Composite Beams. DLR-Mitteilung . pp. 69-83. ISSN 1434-8462

Raja, S and Shashikala, Rajappa and Janardhanam, S and Muthuraj, H Medar and Raghavendra, HM (2009) Experimental Study on gsLVM3 for Transonic Buffet Estimation. In: National Conference on Scientific Achievements of SC & ST Scientists & Technologiests, 14-16 April 2009, Bangalore.

Raja, S and Shashikala, Rajappa and Shankar, V and Janardhanam, S and Vijaya Vittala, NG and Vijayakumar, MP and Bhavana, Jadav (2009) Development of Active Engine Mount System using PZT Actuators for Low Speed Transport Aircraft. Documentation. NAL, Bangalore.

Raja, S and Sinha, PK and Prathap, Gangan and Bhattacharya, Partha (2002) Influence of one and two dimensional piezoelectric actuation on active vibration control of smart panels. Aerospace Science and Technology, 6 (3). pp. 209-216. ISSN 1270-9638

Raja, S and Sinha, PK and Prathap, Gangan and Dwarakanathan, D (2006) Thermally induced vibration control of composite plates and shells with piezoelectric active damping. Smart Materials and Structures, 13 (4). pp. 939-950. ISSN 0964-1726

Raja, S and Sinha, Prasanta K and Prathap, Gangan (2002) Active vibration control of a laminated composite plate with PZT actuators and sensors - An experimental study. In: Conference on Smart Materials, Structures and Systems, 12-14 Dec 2002, Bangalore, India.

Rajagopal, P and Lakshminarayana, HV (1988) Application of Aeroelastic Tailoring in lifting surface design. Project Report. National Aerospace Laboratories, Bangalore.

Rajagopal, P and Ramamurthy, MR (1991) Unsteady airloads and aeroelastic studies of lifting surfaces in transonic flow. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rajagopal, P and Vijaya Vittala, NG (1986) Determination of modal characteristics from random response signal. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rajagopal, P and Vijaya vittala, NG and Somashekar, BR (1988) Aeroelastic tailoring of unswept and forward swept advanced composite wings for divergence costraints. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Rajamohan, -- and Balasubramanian, TS (1975) Estimation of loads and moments on a fully articulated helicopter rotor blade. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rajappa, N and Venkatarangan, P and Viswanathan, KS (1967) The Geomagnetic cavity and the Van Allen radiation belts-II. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rajendran, S and Prathap, Gangan (1999) Eight-node field-consistent hexahedron element in dynamic problems 13; 13;. Structural Engineering and Mechanics, 8 (1). pp. 19-26. ISSN 1225-4568

Raju, Basava B (1966) Vibration of thin elastic plates of linearly variable thickness (Natural frequencies and node patterns for clamped and simply supported square plates of linearly variable thickness solved by finite-difference approximation, using pulsed-air vibrator). International Journal of Mechanical Sciences, 8 (2). pp. 89-100.

Raju, K and Sunder, R (1985) Research and development in the field of fatigue and fracture mechanics at NAL. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Raju, KN (1993) Development of integrated database management and expert system for selection of materials to meet durability and damage tolerance requirements(completion Report). Project Report. National Aerospace Laboratories, Bangalore.

Raju, KN and Sunder, R (1984) Research and development in the field of fatigue and fracture mechanics at the National Aeronautical Laboratory. In: Analysis of Structures - A Commemorative volume published on the occasion of the 60th Anniversary of Dr. S.R.Valluri, Dec 1984, NAL, Bangalore, India.

Ramakrishna, DS and Sathyanarayana, CN and Rajagopal, P and Rajesh, - and Saleem, Syad (1998) Ground vibration testing of HANSA - 3 proto II aircraft. Project Report. National Aerospace Laboratories, Bangalore.

Ramamurthy, MR and Rajagopal, P (1991) Application of Experimental and Theoretical Methods for Prediction of Aeroelastic Characteristics of Swept,13; Tapered and Delta Wings: PAECAST-1. Technical Report. National Aerospace Laboratories, Bangalore, India.

Ramani, TS and Vittala, NGV and Janardhanan, S and Upadhya, AR (1986) Feasibility study of a spring support system for buffet models and a mini shaker for model excitation. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ramesh Babu, C and Prathap, Gangan (1986) Field-consistent two-noded curved axisymmetric shell element. International Journal for Numerical Methods in Engineering, 23 (7). pp. 1245-1261. ISSN 0029-5981

Ramesh Babu, C and Somashekar, BR and Prathap, Gangan (1985) Development of a library of field-consistent finite elements. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ramesh Chandra, . and Gopalan, R and Viswanathan, KS and Aruna, HM (1985) Radome development for Electronic Equipment Pod. Project Report. National Aerospace Laboratories, Bangalore.

Ramesh Chandra, .- and Viswanathan, KS and Gopalan, R (1985) Structural Testing of Radomes '3' and '4' Electronic Equipment Pod, Technical Report Part XI. Project Report. National Aerospace Laboratories, Bangalore.

Rameshbabu, C and Prathap, Gangan (1985) A linear thick curved beam element. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rameshbabu, C and Subramanian, G and Prathap, Gangan (1987) Mechanics of field-consistency in finite element analysis - A penalty function approach. Computers and Structures, 25 (2). pp. 161-173. ISSN 0045-7949

Rameshbabu, C and Subramanian, G and Prathap, Gangan (1985) Mechanics of field-consistency in finite element analysis - a penalty function approach. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rao, Babu MN (1984) Three-Dimensional Stress problem of a finite thick plateE with a through crack under tension.13;. In: 6th International Conference on Fracture (ICF6)., New Delhi, India.

Rao, KVL and Sudha, R and Jagannatha, Rao (1985) A Light Scattering Technique for the Measurement of SMD13; in Sprays. Technical Report. National Aerospace Laboratories, Bangalore, India.

Rao, MNB (1975) Thermal stresses around an elliptic hole in an infinite thick plate subjected to a uniform heat flow. Nuclear Engineering and Design, 35 (2). pp. 299-307. ISSN 0029-5493

Rao, MNB (1976) Thermal stresses around an insulated crack in an infinite plate subjected to a uniform heat flow. International Journal of Fracture, 12 . pp. 777-779. ISSN 0376-9429

Rao, MNB and Guruswamy, P and Rao, MV and Pavithran, S (1977) Studies on vibration of some rib-stiffened cantilever plates. Journal of Sound and Vibration, 57 . pp. 389-402. ISSN 0022-460X

Roshan, Antony and Veera Sesha Kumar, C and Antony, Michael and Jayaraman, M (2011) Structural Design Analysis of a 500 kW Wind Turbine. Project Report. National Aerospace Laboratories, National Aerospace Laboratories.

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Sahoo, PK and Dattaguru, B and Murthy, CRL (2006) Finite Element Analysis of Adhesively Bonded Lap Joints. In: Proceedings of the 14th National Seminar on Aersopace Structures: Fatigue, Fracture and Ageing Structures, 30-31 Jan 2006, Nagpur, India.

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