Items where Author is "Niranjana, T"

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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.

Srikanth kumar, S and Niranjana, T and Rajamurthy, MS and Singh, Suresh K (1992) Estimation Of Roll Derivatives Of A 1/15 Scale LCA Model By Dynamic Wind Tunnel Simulation Technique. Technical Report. NAL, Bangalore.

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.

Madhuranath, P and Niranjana, T (1987) Flight data analysis of the short period characteristics of pushpak aircraft. 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 (1987) A Low Speed Tunnel Semi Free Dynamic Flying Study of Pitching Derivatives of LCA Delta-5 in Active Control using MLE Procedure. Project Report. National Aerospace Laboratories, Bangalore.

Balakrishna, S and Niranjana, T (1987) Wind tunnel dynamic flying study of the pitching moment derivatives of the Standard Dynamics Model in active control. In: AIAA Atmospheric Flight Mechanics Conference, 17-19 Aug 1987, United States.

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 (1986) Moment Stability Derivatives of Prithvi Missile Configuration at Low Speed Using Semi Free Dynamic Flying Method -Proposal. 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.

Padma, Madhuranath and Ramamoorthy, Rajeswari P and Niranjana, T (1978) Ground based vehicle simulation - (Preliminary investigation). 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 Thu Oct 2 03:10:32 2014 IST.