Items where Subject is "AERONAUTICS > Aircraft Design, Testing & Performance"

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Number of items at this level: 272.

A

Ahmed, Sajeer and Selvarajan, S (1991) Investigation of flow field on a hammerhead nose configuration at transonic speeds AIAA-91-1711. In: 22nd Fluid Dynamics, Plasma Dynamics amp; Lasers Conference, 24-26 Jun 1991, Honolulu, Hawaii.

Ananda, CM (2009) Civil aircraft advanced avionics architectures - an insight into saras avionics, present and future perspective. In: International Symposium on Opportunities and Challenges Facing Aviation Industry in Indian Subcontinent, 18-20, 2009, Sreenithi Institute of Science & Technology.

Anantha, KV and Mathur, NB and Krishnan, V (1989) Design characteristics of the variable supersonic nozzle of the base flow facility. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Arokiamary, J and Shanmuga Priya, V and Shanthi Priya, G and Viswamurthy , SR (2012) Fatigue Spectrum for a Stiffened Composite Panel. Project Report. CSIR-NAL, Bangalore.

Aruna, V Murthy and Dattaguru, B and Narayana, HVL and Rao, AK (1990) Improved iterative finite element solution for pin joints. Computers and Structures, 36 (6). pp. 1121-1128.

Arunkumar, V and Paranjpe, Promod A (1979) Experimental evaluation of damping coeficient of a squeeze film mounted ball bearing AIAA-79-7013. In: 4th International symposium on Air breathing engines.

Ashbaugh, NE and Dattaguru, B and Khobeib, M and Nicholas, T and Prakash, Raghu V and Ramamurthy, TS and Seshadri, BR and Sunder, R (1995) Elastic-Plastic Finite Elament Analysis of Fatigue Crack Closure in an Aluminium-Copper Alloy Part-11:. Technical Report. National Aerospace Laboratories, Bangalore, India.

Ashok, G (1991) Calculation of the Aerodynamic Tail Loads for NALLA. Technical Report. National Aerospace Laboratories, Bangalore, India.

Ashok, G and Karthik, K and Rohidekar, R Satish (1992) NALLA 2: Data Report. Technical Report. National Aerospace Laboratories, Bangalore, India.

B

Babu, Lakshman B (2000) PC Based Data Acquisition and Processing Softwarefor Force and Pressure Measurements in 1 .5m Low Speed Wind Tunnel13;. Technical Report. National Aerospace Laboratories, Bangalore, India.

Balakrishna, S (1976) Time domain and time series models for human activity in compensatory tracking experiments. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Balakrishna, S (1983) A low speed tunnel for studies on active control of scaled models. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Balakrishna, S and Niranjana, T (1987) Wind tunnel dynamic flying study of the pitching movement derivatives of the standard dynamics model in active control AIAA-87-2626. In: AIAA atmospheric flight mechanics conference.

Balakrishna, S and Niranjana, T and Rajan, SR Moment stability Derivatives of N A G Missile Configuration-at Low Speed using Semi-free Dynamic Flying. Project Report. NAL, Bangalore.

Balasingh, C and Govindarajaswamy, K and Krishnan, A and Raghumurthy, T and Ramesh, TG and Shubha, V and Singh, AK and Subbarayadu, K and Rao, Venkata (1991) Design and fabrication of a mobile x-ray stress 13; diffractometer. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Balasubramanian, TS and Savanur, Satyendra and Sharma, Naresh and Murthy, MVE and Rao, KP and Damania, RB (1990) Design of GFRP wing of NAL's Light Aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Bandyopadhyay, K (1991) Development of transducers for aerospace structure testing using piezoelectric ceramic/polymer. Part 1 : Fabrication of accelerometer using piezoelectric ceramic. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Bandyopadhyay, K (1989) Preparation and testing of piezoelectric polymer component for making transducers. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Basappa, - and Jategaonkar, RV (1995) Aspects of Feed Forward Neural Network Modeling and its Application to Lateral-Directional Flight Data. Technical Report. National Aerospace Laboratories, Bangalore, India.

Basappa, - and Jategaonkar, RV (2003) Evaluation of recursive methods for aircraft parameter estimation. Technical Report. National Aerospace Laboratories, Bangalore, India.

Bera, Rajendra K (1990) Human factors in fighter software development. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Bera, Rajendra K (1974) Some remarks on the solution of the lifting line equation. Journal of Aircraft, 11 (10). pp. 647-648. ISSN 0021-8669

Bera, Rajendra K (1990) A conceptual framework for fighter flight control systems. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Bera, Rajendra K and Ramachandra, SM (1979) Conically cambered delta wings in supersonic flow. I - Basic solutions. Journal of Aeronautical Society of India, 29 (3, 4). pp. 87-94.

Bera, Rajendra K and Ramachandra, SM (1974) Method of orthogonal loadings - A fresh look. Journal of Aircraft, 11 (10). pp. 650-651.

Bera, Rajendra K and Ramachandra, SM (1976) Some theorems concerning drag minimization. Revue Roumaine des Sciences Techniques, Serie de Mecanique Appliquee, 21 . pp. 523-529.

Brahma, KK (1998) Seismic Qualification testing of 250AH and 750AH Cells on Steel rack. Technical Report. National Aerospace Laboratories, Bangalore, India.

Brahma, KK (1998) seismic Qualification Testing of 250V DC, 100 KW Standby Battery Charger. Technical Report. National Aerospace Laboratories, Bangalore, India.

Brahma, KK and Parida, BK (1999) Buffet Response Studies of An Aircraft. Technical Report. National Aerospace Laboratories, Bangalore, India.

C

Chakravarathy, R and Anupama, - (1992) Pitot static system. Project Report. National Aerospace Laboratories, Bangalore.

Challappa, KR (1992) LTA wing structure - Option 1. Project Report. National Aerospace Laboratories, Bangalore.

Chandra, S (1999) The structure of a physical behaviour description facility. Artificial Intelligence in Engineering, 13 (1). pp. 91-103.

Chandrakala, K and Vanaja, A and Rao, RMVGK (2007) SOME PRELIMINARY STUDIES ON THE SHELF LIFE OF RT CURE GLASS-EPOXY PREPREG. Project Report. National Aerospace Laboratories, Bangalore.

Chattopadhyay, Lalitha (2011) Analytical solution for bending stress intensity factor from Reissner's plate theory. Engineering, 3 (5). pp. 517-524.

Chetty, Shyam (1988) Design of robust flight control systems. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Chetty, Shyam and Deodhare, Girish (2002) Design and development of flight control laws for LCA. Journal of Aeronautical Society of India, 54 (2). pp. 142-144.

Chetty, Shyam and Henschel, F (1990) Model Following Control System Design - Preliminary ATTAS In-flight Simulation Test Results. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Chetty, Shyam and Usha, UN (1989) Design of Stability Augmentation Systems using Vector Optimisation Techniques. Project Report. NAL, Bangalore.

Civil Aviation Unit, Civil Aviation Unit (1990) Proposal on Design and Development of LTA. Project Report. NAL, Bangalore.

D

Damania, RB (1986) Concept Study For a 80% Scaled Derivative LCA. Project Report. National Aerospace Laboratories, Bangalore.

Damania, RB and Karthik, K and Kumar, Mahesh and Aravamudhan, Srikanth (1991) Design of the main landing gear for the NALLA prototype. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Damania, RB and Varute, PT (1991) Proposed modifications/improvements to the draft specifications of DGCA, New Delhi, on requirements for airworthiness certification of experimental aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Desai, SS (1993) CFD and some of its applications. In: Recent advances in aerospace sciences and engineering; Proceedings of the International Symposium, 12-15 Dec 1992, Bangalore, India.

Desai, SS and Rangarajan, R (1987) Viscous transonic flow over aerofoils using transonic full potential equation in a system of cartesion coordination AIAA-87-411. In: AIAA 25th aerospace science meeting, 12-15, Jan 1987, Reno, Nevada.

Desai, SS and Rangarajan, R and Singh, JP and Ravichandran, KS (1987) Full potential flow computations using cartesian grids. In: AIAA 8th Computational Fluid Dynamics Conference.

Deshpande, MD and Srinidhi, BG (2003) Natural Convection in a Cavity of Large Aspect Ratio. Technical Report. National Aerospace Laboratories, Bangalore, India.

Desikan, KS (1974) Design of a force balance calibration rig. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Dutt, HNV (1985) Parametric bi-cubic surface patch for computer aided geometric design of aircraft and/or other three-dimensional geometries. Technical Report. National Aeronautical Laboratory, Bangalore, India.

F

FMCD, - (2004) Progress in Ramp;D, T of Flight Mechanics and Control Division 2004 - 2005. Technical Report. National Aerospace Laboratories, Bangalore, India.

G

Geeta, KS and Renuka Devi, M and Krishnan, A (1997) Structural Methodology of Software Development a Case Study Braider Controller. Technical Report. National Aerospace Laboratories, Bangalore, India.

Girija, G (2004) Multi sensor data fusion for sensor failure detection and13; health monitoring for Aerospace applications- A brief survey. Technical Report. National Aerospace Laboratories, Bangalore, India.

Girija, G and Parameswaran, V and Raol, JR (1991) Determination of aircraft performance from flight data. In: National Seminar on quot;Flight Testingquot;, 26-27 Apr 1991, ASTE, Bangalore.

Girija, G and Parameswaran, V and Raol, JR (1991) Determination of aircraft performance from flight data. In: National Seminar on quot;Flight Testingquot;, 26-27 Apr 1991, ASTE, Bangalore.

Girija, G and Raol, JR (2001) Comparison of methods for association and fusion of multi sensor data for tracking applications 13; 13;. In: AIAA Guidance, Navigation, and Control Conference and Exhibit, 6-9 Aug 2001, Montreal, United States.

Gopalan, R and Chandra, Ramesh (1989) Environmental effects on composite structures. Journal of Aeronautical Society of India, 41 (1). pp. 55-59.

Gopalratnam, Girija and Raol, JR and Jategaonkar, RV (1993) Aerodynamic parameter estimation from dynamic maneuvers by two step methodology. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Gopinath, R (1985) Wall Interference Studies in 3-D Flows. Technical Report. National Aerospace Laboratories, Bangalore, India.

Gur, Ohad and Lazar, Gali and Yaniv, Aharon and Burman, Abhishek (2011) Multidisciplinary Analysis for a Civil Aircraft Conceptual Sizing. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.

H

Henschel, Frohmut and Chetty, Shyam (1987) An improved design technique for model following control13; systems in quot;In-flight simulationquot;. Technical Report. National Aeronautical Laboratory, Bangalore, India.

I

Ismail, Shaik and Chetty, Shyam (1992) Ideal Aircraft Handling Quality Models Longitudinal Axis. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ismail, Shaik and Parameswaran, V and Shyam, Chetty (1998) Handling Qualities Analysis of Flight Test Data of13; Fighter Trainer Aircraft MiG 21 Type 69b U-2153 Using HQPACK. Technical Report. National Aerospace Laboratories, Bangalore, India.

Ismail, Shaik and Singh, Jatinder (2004) HELI-HQPACK Version 1.0. Technical Report. National Aerospace Laboratories, Bangalore, India.

Ismail, Shaik and Singh, Jatinder (2005) Nonlinear aerodynamic global model indentification using Gram-Schmidt orthogonalisation13;. Journal of Aerospace Sciences and Technology, 57 (4). pp. 392-400. ISSN 0972-950X

Ismail, Shaik and Von Gruenhagen, Wolfgang and Harriers, Mario and Pausder, Heinz-Juergen (2003) HAT:Handling-qualities analysis toolbox for rotorcraft and aircraft. In: 29th European Rotorcraft Forum, 16-18 Sep 2003, Friedrichshafen, Germany.

Ismail, shaik (1988) Model simplification based on the concept of equivalent dead time. Technical Report. National Aeronautical Laboratory, Bangalore, India.

J

Jategaonkar, RV and Balakrishna, S (1986) Effects of flap position on longitudinal parameters of HFB-320. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Jatinder, Singh (1998) Parameter Estimation for Aircraft Flying in Turbulence. Technical Report. National Aerospace Laboratories, Bangalore, India.

Jayasankar, S and Dayananda, GN and Varughese, Byji and Kumar, Senthil P SMA Based Adaptive Concept on Wings of Large Civil Aircraft. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD-2009) December 10-12, 2009, Bangalore, India, 10-12 Dec 2009, Bangalore, India.

Jha, RM (1994) Determination of Optimal Antenna Location on Aircraft Structures. Project Report. NAL, Bangalore.

Jinde, P and Rajeev, G and Nagpal , Ankur (2011) Design of a special twin sting support system for force measurements on a launch vehicle model. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.

Jugseniya, Chandrakant B and Pashilkar, Abhay A (2005) Thermodynamic Analysis of Turbofan Engine. Technical Report. National Aerospace Laboratories, Bangalore, India.

K

Kailas, SV and Narasimha, R (1999) The eduction of structures from flow imagery using wavelets. I - The mixing layer. Experiments in Fluids, 27 (2). pp. 167-174. ISSN 0723-4864

Kanagarajan, V and Arokkiaswamy, A (1986) Experimental Studies on a 1/12 Scale Model of Prithvi Missile. Project Report. NAL, Bangalore.

Kanakamuthu, - and Rajeev, KT and Chandra, AP and De, Manabendra M (2011) Aerodynamic design of the 500 W wind turbine rotor/blade. Technical Report. National Aerospace Laboratories, Bangalore, India.

Kannan, TS and Saravana, BV (1980) Design and fabrication of a laboratory scale tape coating unit. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Kashyap, SK and Girija, G and Raol, JR (2004) Evaluationof Converted Measurement. andModified13; Extended. KalmanFilters for Target Tracking. Technical Report. National Aerospace Laboratories, Bangalore, India.

Kashyap, SK and Naidu, VPS and Singh, Jatinder and Girija, G and Raol, JR (2004) Multiple target tracking using IMMPDAF Filter. In: National Workshop on Tactical Guidance, DRDL, 2004, Hyderbad.

Kashyap, Sudesh and Girija, G (1999) Implementation Aspects of Dynamic Tracking Filter amp; Fusion Filter a Typical Flight Test Range. Technical Report. National Aerospace Laboratories, Bangalore,India.

Kashyap, Sudesh Kumar and Raol, JR (2004) Fuzzy Logic Based Adaptive Filter for Target Tracking in Presence of Glint Noise. Technical Report. National Aerospace Laboratories, Bangalore, India.

Kavitha, K and Rajalakshmi, - and Raol, JR (1997) Kalman Filtering for Target Tracking. Technical Report. National Aerospace Laboratories, 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.

Khare, Alok and Madhuranath, Padma (1993) Linear simulation software LINSIM. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Khatri, AK and Jatinder, Singh and Sinha, NK (2012) Aircraft maneuver design using bifurcation analysis and sliding mode control techniques. Journal of Guidance, Control and Dynamics, 35 (5). pp. 1435-1449. ISSN 0731-5090

Kidambi, R and Shankar, PN (2005) The effects of the contact angle on sloshing in containers. Proceedings of the Royal Society of London, 460 (2048). pp. 2251-2267. ISSN 1364-5021

Krishnamurthy, K and Wulff, G (1993) DIVA on PC Part 1: Analysis of time-dependent data. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Krishnamurthy, M and Prabhudesai, V and Panda, GK (2001) On the upper limit of the Oswaldx2019;s efficiency factor for an airplane. Journal of Aeronautical Society of India, 53 (4). pp. 203-205.

Krishnan, V and Kangovi, S and Yajnik, KS and Balasubramaniam, R (1978) Design of a balance for NAL base flow facility. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Kumar, Mohan and Samiullah, TH and Rao, RMVGK (2006) Fabrication highlights of domes for the Air Combat Simulator (ACS) for ARDC (HAL)/IAF. Project Report. National Aerospace Laboratories, Bangalore.

Kumar, Mohan and Samiullah, TH and Rao, RMVGK (2006) Tooling development of domes for the Air Combat Simulator (ACS)for ARDC (HAL)/IAF. Project Report. National Aerospace Laboratories, Bangalore.

Kumar, Rajeeva (1997) Failure detection, isolation and estimation for flight control surfaces and actuator. Technical Report. National Aerospace Laboratories, Bangalore, India.

Kumar, Shiva BR and Shantha Kumar, N and Raol, JR (1997) User Manual for Alpha DEC systems of S1 Lab. Technical Report. National Aerospace Laboratories, Bangalore, India.

Kumari, Asha and Kotresh, Gaddikeri M and Byji, Varughese (2010) Stress Analysis of Ailerons-control bracket attachment to front-spar in SARAS composite wing. Project Report. NAL, Bangalore.

Kumari, Asha and Kotresh, Gaddikeri M and Byji, Varughese (2010) Stress Analysis of Composite wing of SARAS Aircraft at extreme operating temperatures. Project Report. NAL, Bangalore.

Kumari, Asha and Murali Krishna, D and Kotresh, Gaddikeri M and Byji, Varughese (2010) Local 3-D stress analysis of metallic front and rear landing gear beams of SARAS-composite wing. Project Report. NAL, Bangalore.

L

Lakshman Babu, B and Suryanarayana, GK (2000) A Method for Measurement of Massflow Rate Through Supersonic13; Air-intake Model in Wind Tunnel Tests. Technical Report. National Aerospace Laboratories, Bangalore, India.

Lakshminarayana, HV and Godbole, A (1974) Finite element analysis of laminated anisotropic shell structures. In: Seminar on the Role of Computers in Structural Analysis, Design and Optimisation, 13-14 June 1974, Bangalore, India.

Lakshminarayana, HV and Murthy, MVV (1976) On stresses around an arbitrarily oriented crack in a cylindrical shell. International Journal of Fracture, 12 . pp. 547-566. ISSN 0376-9429

Lathasree, P and Pashilkar, AA (2011) Digital Simulation Model for Turboprop Engine. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.

M

Madhava Rao, C and Raj Mahindra, - and Nagaraja Rao, TG (1992) Economic study of an integrated civil aircraft development, production and overhaul programme. Project Report. National Aerospace Laboratories, Bangalore.

Madhavan, Chinmayee and Dasannacharya, BS and Rajanna, D and Nagabhushana, S (1985) Aircraft weighing system. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Madhuranath, Padma and Parameswaran, V and Raol, JR and Krishnamuthy, K (1991) Flight testing for aircraft modelling. In: National Seminar on Flight Testing, 26-27 Apr 1991, Bangalore.

Madhuranath, Padma and Sridhar, JK and Bhagavan, Satya B (1987) Simulation of a Light Aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Madhuranath, Padma and Sridhar, JK and Satyabhagavan, B (1989) Flight Simulation of HS-748 with and without rotodome PArt 2 - Rolls Royce Engine Simulation. Project Report. NAL, Bangalore.

Madhuranath, Padma and Sridhar, JK and Srinath Sastry, CV (1989) Flight Simulation of HS - 748 with and without rotodome Part 3- Aerostatic Model Formulation. Project Report. NAL, Bangalore.

Mahadevan, Chinmayee and Rao, Dhruva NS and Murthy, NN (1996) Environmental Conditions and Test Procedures for Airborne Equipment - A Comprehensive guide to Aircraft Systems Designers. Technical Report. National Aerospace Laboratories, Bangalore, India.

Mahishi, JM and Chandra, Ramesh and Murthy, MVV (1980) Transient heat conduction analysis of laminated composite nose cone. Journal of Aeronautical Society of India, 32 . pp. 77-84.

Majumdar, Sekhar and Zhu, J and Rodi, W (1990) Calculation of three-dimensional turbulent flow around ship13; structures. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Manjunath, B and Nandini, - and Sreenivasan, KG and Renuka Devi, M and Krishnan, A (1997) Software Testing Paradigm for Safety13; Critical Software. Technical Report. National Aerospace Laboratories, Bangalore,India.

Manoharan, LC (1985) Development of a fiberoptic data bus for fly-by-light application on aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Mozumdar, S and Patel, TS (1980) Investigation on rotating ailerons. Aeronautical Society of India, Journal, 32 . pp. 1-5.

Muralidhara, HS and Shembharkar, TR and Pai, BR and Ramanujam, PS and Jayaprakash, GN and Pandey, PK (2001) Cold flow analysis of an aero-engine gas turbine combustor configuration 13; 13;. In: International Symposium on Air Breathing Engines, 3-7 Sept 2001, Bangalore, India.

Murthy, AV (1974) Hypersonic flow over blunted slender wedges. Journal of Aircraft, 11 . pp. 649-651. ISSN 0021-8669

Murthy, NN (1987) Microprocessor based 32 channel PCM telemetry system. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Murthy, Satyanarayana PV (2003) Adaptive non-linear flight controller using neural networks for unmanned helicopter. Technical Report. National Aerospace Laboratories, Bangalore, India.

N

Naganarayana, BP and Mohan, P Rama and Prathap, Gangan (1997) Accurate thermal stress predictions using CxB0;-continuous13; higher-order shear deformable elements. Computer Methods in Applied Mechanics and Engineering, 144 (1-2). pp. 61-75.

Naganarayana, BP and Prathap, Gangan (1991) Field-consistency analysis of 27-noded hexahedral elements for constrained media elasticity. Finite Elements in Analysis and Design, 9 (2). pp. 149-168.

Naganarayana, BP and Prathap, Gangan and Dattaguru, B and Ramamurty, TS (1992) Field-consistent and variationally correct representation of transverse shear strains in the nine-noded plate element. Computer Methods in Applied Mechanics and Engineering, 97 (3). pp. 355-374.

Nagpurwala, QH (1987) Design and calibration of three hole cylinderical13; combination probes. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Naidu, VPS and Girija, G (2005) Fusion of Radar and Infrared Search amp; Track Sensor Data using Kalman Filter. Technical Report. National Aerospace Laboratories, Bangalore, India.

Naidu, VPS and Girija, G and Raol, JR (2005) Estimation of Launch and Impact Points of a Flight Trajectory using UD Kalman Filter/Smoother. Technical Report. National Aerospace Laboratories, Bangalore, India.

Nair, Ravindranath U and Jha, RM (2004) Novel design for a monolithic hybrid variable thickness radome (hy-VTR). IEEE Antennas and Propagation Society, 1 . pp. 878-881.

Nandanan, M and Ramaswamy, MA (1985) Supercritical wing design for combat aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Narasimhan, SV and Harish, M (2006) Spectral estimation based on discrete cosine transform and13; modified group delay. Signal Processing, 86 . pp. 1586-1596.

National Aerpspace Laboratories, Bangalore, India (2008) The Mandate. [Image]

Nirmala, GA and Ramamoorthy, P and Damania, RB (1988) Validation and extension of NCSU code for path performance of a small aircraft and its application to LCRA. Technical Report. National Aeronautical Laboratory, Bangalore, India.

P

Padma, Madhuranath and Ramamoorthy, Rajeswari P and Niranjana, T (1978) Ground based vehicle simulation - (Preliminary investigation). Technical Report. National Aeronautical Laboratory, Bangalore, India.

Padmavathi, T and Jyotsna, T.S and Rao, RMVGK DEVELOPMENT OF SPECIALITY RESINS FOR RADOME APPLICATIONS. Project Report. National Aerospace Laboratories, Bangalore.

Parameswaran, V and Jategaonkar, RV (2001) Calibration of 5 - Hole Probe for Flow Angles from ATTAS Flight Data. Technical Report. National Aerospace Laboratories, Bangalore, india.

Parameswaran, V and Jategaonkar, RV (2003) Calibration of air data systems using DGPS based kalman filtering. Technical Report. National Aerospace Laboratories, Bangalore, India.

Parameswaran, V and Plaetschke, E (1990) Flight path reconstruction using extended kalman filtering techniques. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Parameswaran, V and Raol, JR (2002) Evaluation of attitude determination methods for aircraft using GPS signals13;. In: 9th Saint Petersting International conference, 27-29 May 2002, Russia.

Parameswaran, V and Raol, JR and Madhuranath, Padma (1993) Mathematical model building from flight data for simulation validation of a modified aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Parameswaran, V and Umesh, BN (2001) Attitude Determination of Aircraft Using GPS Signals. Technical Report. National Aerospace Laboratories, Bangalore, India.

Parida, BK and Nicholas, T (1994) Elevated temperature fatigue crack growth behavior of Ti-1100. Fatigue and Fracture of Engineering Materials and Structures, 17 (5). pp. 551-561.

Pashilkar, AA (2002) Surface Pressure Estimates for Pitching Aircraft Model at High Angles-of-attack13; 13;. Defence Science Journal, 52 (4). pp. 417-427.

Pashilkar, AA and Pradeep, S (2001) Computation of flight mechanics parameters using continuation techniques. Journal of Guidance, Control and Dynamics, 24 (2). pp. 324-329.

Pavan Kumar, DVTG (2004) Analysis of Composite End Notch Flexure Specimen using13; Various Plate Theories. Project Report. National Aerospace Laboratories, Bangalore, India.

Pavan Kumar, DVTG and Raghu Prasad, BK (2003) Higher-Order Beam Theories for Mode II Fracture of Unidirectional Composites. Journal of Applied Mechanics, Transactions ASME, 70 (6). pp. 840-852.

Pavan Kumar, DVTG and Selvaraj, R (2004) Analysis of Composite Double Cantilever Beam Specimen using13; Various Plate Theories. Project Report. National Aerospace Laboratories, Bangalore, India.

Prabhu, KR (1976) Drag prediction methods for prelimanary design of an aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prabhu, KR (1976) Drag prediction methods for preliminary design of an aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prakash, M. Rajendra and Murgan, Senthil and Rao, RMVGK (2007) NDT and Post Cure Report on HANSA-3 Aircraft Composite Components - Sl.No. 011. Project Report. National Aerospace Laboratories, Bangalore.

Prakash, M. Rajendra and Rao, RMVGK (2007) On Field Inspection of HANSA-3 Aircraft (VT-HNS) at IIT - Kanpur. Project Report. National Aerospace Laboratories, Bangalore.

Prakash, M.Rajendra and Rao, RMVGK (2006) NDT and Post Curing of Composite Airframe Components of HANSA-3 Production Aircraft (VT-HOC and TH-001). Project Report. National Aerospace Laboratories, Bangalore.

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

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

Prathap, Gangan and Naganarayana, BP (1995) Consistent thermal stress evaluation in finite elements. Computers and Structures, 54 (3). pp. 415-426.

Prathap, Gangan and Naganarayana, BP (1992) Field-consistency rules for a three-noded shear flexible beam element under non-uniform isoparametric mapping. International Journal for Numerical Methods in Engineering, 33 (3). pp. 649-664.

Prathap, Gangan and Nirmala, K (1990) Finite element formulations of constrained media elasticity. A bibliography. Finite Elements in Analysis and Design, 7 (3). pp. 253-270.

Prathap, Gangan and Shashirekha, BR (1993) Variationally correct assumed strain field for the simple curved beam element. Computers and Structures, 47 (6). pp. 1071-1073.

Prathap, Gangan and Somashekar, BR (1988) FIELD- AND EDGE-CONSISTENCY SYNTHESIS OF A 4-NODE QUADRILATERAL PLATE BENDING ELEMENT. International Journal for Numerical Methods in Engineering, 26 (8). pp. 1693-1708.

R

Raghavendra Rao, S and Manyam Kothapalli, S.R.S and Ravishankar, S (2014) Study of Bend Angle Allowance for Sheet Metal Forming in Aerospace Industry. In: International Conference on Trends in Product Life Cycle, Modeling Simulation and Synthesis PLMSS-2014, 6th to 8th January 2014, Vellore Institute of Technology, Vellore, TamilNadu, India.

Raja, S and Dwarakanathan, D and Sinha, PK and Prathap, Gangan (2004) Bending behavior of piezo-hygrothermo-elastic smart laminated composite flat and curved plates with active control. Journal of Reinforced Plastics and Composites, 23 (3). pp. 265-290.

Raja, S and Sreedeep, R and Prathap, Gangan (2004) Bending behavior of hybrid-actuated piezoelectric sandwich beams. Journal of Intelligent Material Systems and Structures, 15 (8). pp. 611-619.

Rajakumar, A and Jharia, Anoop and Subba Rao, M (1990) A preliminary report on LCA fin design13; 13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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