Items where Author is "Rajan, SR"

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Number of items: 10.

Kumar, Vineet and Panda, GK and Rajan, SR and Khatri, AK and Sahoo, S (2008) Few aspects of flight data acquisition and analysis for twin turboprop Saras aircraft. In: Proceedings of the International Conference on Aerospace Science and Technology (INCAST 2008-098), 26-28 Jun 2008, Bangalore, India.

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.

Rajamurthy, MS and Rajan, SR and Basappa, - and Niranjana, T (1993) Estimation Of Longitudinal Moment Derivatives Of Missile Configuration Using Semi Free Flying Technique. Technical Report. NAL, Bangalore.

Balakrishna, S and Niranjana, T and Rajamurthy, MS and Srinathkumar, S and Rajan, SR and Singh, Suresh K (1993) Estimation of aerodynamic derivatives using Dynamic Wind Tunnel Simulation Technique. In: Symposium on System identification, 24-25 Nov 1993, Bangalore, India.

Balakrishna, S and Niranjana, T and Rajan, SR (1992) A rotary derivative rig for FMCD low speed tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Balakrishna, S and Niranjana, T and Rajan, SR (1991) Augmentation of the 1.2m x 1.2m low speed dynamic test wind tunnel at NAL. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Balakrishna, S and Niranjana, T and Rajan, SR and Rajamurthy, MS (1991) Dynamic flying investigations on 1/13.5 NALLA Model (Longitudinal Results). Technical Report. National Aeronautical Laboratory, Bangalore, India.

Karunakar, K and Murthy, NN and Niranjana, T and Rajan, SR and Shyam Chetty, and Padma, Madhuranath and Shylaja, G Prasad (1987) Design and simulation of a Digital Combat Flap controller for a fighter Aircraft. Project Report. National Aerospace Laboratories, Bangalore.

Balakrishna, S and Niranjana, T and Rajan, SR (1986) A low speed tunnel semi-free dynamic flying study of the high angle of attack pitch derivatives of HF-24 using MILE procedure. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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.

This list was generated on Wed Sep 3 02:29:13 2014 IST.