Items where Author is "Rajagopal, P"

Book / Book Chapter

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

Conference or Workshop Item

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.

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)

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.

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.

Journal Article

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.

Proj.Doc/Technical Report

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.

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 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.

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.