Items where Author is "Viswanath, S"

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Number of items: 35.

Conference or Workshop Item

Chandra, N and Ananda, CM and Shivaprasad, MV and Rajan, SR and Krishna, Saraswathi and Shivaprasad, S and Venkatasubramanyam, DV and Viswanath, S (2008) In-flight vibration and temperature measurements on a typical aircraft for test tailoring. In: International Conference on Aerospace Science and Technology (INCAST 2008-094), 26-28 Jun 2008, Bangalore, India.

Viswanath, S and Chandra, Satish and Biswas, Kanchan (2006) Development of Vibration Specifications for LRUs on Fighter Aircraft from Flight Data. In: Proceedings of the 14th National Seminar on Aerospace Structures: Fatigue, Fracture and Ageing Structures, 30-31 Jan 2006, Nagpur, India.

Murthy, MVV and Raju, KN and Viswanath, S (1979) On the bending stress distribution at the tip of a stationary crack from Reissner's theory. In: Proceedings of the International Conference on Fracture Mechanics in Engineering Application, 26-30 Mar 1979, Bangalore, India.

Lakshminarayana, HV and Viswanath, S (1978) Application of the finite element method to the analysis of laminated composite shell structures. In: Symposium on Applications of Computer Methods in Engineering, 23-26 Aug 1977, California, USA.

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.

Viswanath, S and Murthy, MVV and Rao, KP Finite element analysis of plates with through cracks from higher order plate theory. In: Sixth International Conference on Fracture (ICF6), 4-10 Dec 1984, New Delhi, India.

Journal Article

Chattopadhyay, Lalitha and Murthy, Sridhara S and Viswanath, S (2007) Exact solution for bending of an elastic plate containing a crack and subjected to a concentrated moment. International Journal of Computational Methods, 4 (2). pp. 265-281. ISSN 1793-6969

Subramanya, HY and Viswanath, S and Narasimhan, R (2007) Influence of crack tip constraint on void growth in pressure sensitive plastic solids-1: 2D analysis. Engineering Fracture Mechanics, 75 . pp. 1045-1063.

Subramanya, HY and Viswanath, S and Narasimhan, R (2005) A three-dimensional numerical study of mixed mode (I and II) crack tip fields in elastic-plastic solids. International Journal of Fracture, 136 (1-4). pp. 167-185. ISSN 0376-9429

UdayaKumar, A and Vyjayanthi, N and Venu, PG and Kannan, TS and Narayana, R and Viswanath, S (2003) Weibull analysis of modulus of rupture of the slip-cast amorphous silica (SCAS) determined by the 4-point bending test. InterCeram: International Ceramic Review, 52 (2). pp. 90-94.

Viswanath, S and Lakshminarayana, HV and Ravindranath, DD (1989) A modified crack closure integral method for calculating stress intensity factors for cracked plates subject to bending loads. International Journal of Fracture, Vol. 4 . R45-R50. ISSN 0376-9429

Viswanath, S and Murthy, MVV and Krishnamurthy, AV and Rao, KP (1989) A special crack tip element for bending of plates with through cracks from a sixth-order plate theory. Engineering Fracture Mechanics, Vol. 3 (01). pp. 91-109. ISSN 0013-7944

Murthy, MVV and Viswanath, S and Rao, krishna Murty (1988) Two-dimensional model for crack closure effect in plates under bending 13; 13;. Engineering Fracture Mechanics, 29 (4). pp. 435-452. ISSN 0013-7944

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

Viswanath, S and Prathap, Gangan (1983) A note on locking in a shear flexible triangular plate bending element. International Journal for Numerical Methods in Engineering, 19 (2). pp. 305-309. ISSN 0029-5981

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

Viswanath, S and Murthy, SS and Shah, CG (1980) Finite element analysis of some aerospace shell structures. Aeronautical Society of India, Journal, 32 . pp. 109-115.

Lakshminarayana, HV and Viswanath, S (1978) A high precision triangular laminated anisotropic cylindrical shell finite element. Computers and Structures, 8 . pp. 633-640. ISSN 0045-7949

Proj.Doc/Technical Report

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.

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.

Somenath , Mukharjee and Prakssh Shashi , B M and Alok Burgul , P and Shivaprasad, MV and Krishna , Saraswathi and Viswanath, S (2007) A Method for Dynamic Characterization and Response Prediction Using Ground Vibration Test(GVT)Data for Unknown Structures. Technical Report. NAL, Bangalore.

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.

Sathyanarayana, CN and Ramakrishna Parsad, BH and Venkatasubramanyam, DV and Chinmayee , Madhavan and Viswanath, S (2004) Vibration Qualification Tests on Fatigue Meter. Project Report. National Aerospace Laboratories, Bangalore.

Sathyanarayana, CN and Krishna, Saraswathi and Dwarakanath, K and Nagaraja, BV and Vijaya Kumar, PS and Vijaya Vittala, NG and Viswanath, S and Shashikant, AK (2004) Ground Vibration Testing of SARAS Aircraft. Technical Report. National Aerospace Laboratories, Bangalore, India.

Vijaya Vittala, NG and Barai, A and Kamesh, JV and Viswanath, S and Somashekar, BR (1994) Flutter Characteristics of HANSA2 (NALLA 2C). Technical Report. National Aerospace Laboratories, Bangalore, India.

Jayatheertha, C and Viswanath, S (1992) Static buckling and free vibration analysis of composite/ sandwich plates using improved transverse shear stiffness. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Viswanath, S and Mahasenan, N (1992) LAMPRO : A PC-based software for the design of reinforcements for cutouts in composite laminates. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sridhara Murthy, S and Jayatheertha, C and Viswanath, S and Gopalaksrishnan, . and Murthy, MVV (1989) Static Analysis of rotodomed Aircraft Part II: Result. Project Report. National Aerospace Laboratories, Bangalore.

Sridhara Murthy, S and Viswanath, S and Gangan , .Prathap (1988) Static Analysis of Rotodomed aircraft Part II: Results for vertical gust load case (vB1). Project Report. National Aerospace Laboratories, Bangalore.

Viswanath, S (1985) An Overview of General Purpose Program Packages at NAL. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Ramanathan, R and Viswanath, S (1963) A study of hourly wind speeds at New Delhi from the point of view wind power utilisation. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ramanathan, R and Viswanath, S (1963) A study of the hourly wind speeds at Jodhpur from the point of view of mind power utilization. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ramanathan, R and Viswanath, S (1963) A study of the hourly wind speeds at Jodhpur from the point of view of wind power utilization. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Janardhan, S and Viswanath, S (1963) A study of the hourly wind speeds at Gopalpur from the point of view of wind power utilization. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ramanathan, R and Viswanath, S (1963) A study of the hourly wind speed at Lucknow from the point of view of wind power utilization. Technical Report. National Aeronautical Laboratory, Bangalore, India.

This list was generated on Fri Aug 1 04:00:26 2014 IST.