Items where Author is "Rajagopal, P"

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Number of items: 18.

Shankar, V and Rajagopal, P and Shashikala, Prakash and Nagaraja , BV and Vijayakumar, PS (1999) Design and Development of Instrumentation for Active Vibration Control of Smart Aerospace Structures. In: Proceedings of the International Conference on Smart Materials, Structures and Systems, 7-10 July 1999, Ninth National Seminar on Aerospace Structures.

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.

Somashekar, BR and Rama Murthy, MR and Rajagopal, P and Sundararajan, D and Shashikala, Rajappa and Annamma Samuel, - and Janardhanam, S (1997) Aeroelastic testing of LCA wing models - Model fabrication - Ground testing - Wind tunnel testing and Data analysis. Project Report. National Aerospace Laboratories, Bangalore.

Rajagopal, P and Raja, S and Antony, Michael and Arunkumar, V (1995) Analytical and Experimental studies on cantilever type squeeze film Dampers. In: Fourth India MSC user’s conference. (Submitted)

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

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.

Ramamurthy, MR and Rajagopal, P (1991) Application-of experimental and theoretical methods for13; prediction of steady and unsteady loads on flexible swept, tapered and delta wings: PALAST-1. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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

Vijaya Vittala, NG and Rajagopal, P and Madhusudan, BS (1990) Analysis of a Cantilivered Cylindrical Squeeze Film Damper. Project Report. National Aerospace Laboratories, Bangalore.

Vijaya Vittala, NG and Rajagopal, P (1990) Dynamic and flutter analysis of GFRP wing of NAL's light aircraft13; 13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rajagopal, P and Vittala, NGV and Ramani, TS (1990) Aeroelastic analysis of a low aspect ratio wing. Journal of Aeronautical Society of India, 42 . pp. 51-56.

Rajagopal, P and Vittala, NGV and Ramani, TS (1990) Aeroelastic analysis of a low aspect ratio wing 13; 13;. In: 40th Aeronautical Society of India, Annual General Meeting,, 19-20 Dec 1988, Madras, 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.

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.

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

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

Arunkumar, V and Rajagopal, P (1985) Computer program for prediction of DMPED critical speeds of rotor systems. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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

This list was generated on Thu Nov 27 03:34:37 2014 IST.