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T Niranjana
Observed names:
Niranjana, T,
T. NIRANJANA,
T. Niranjana
Institution:
ViGYAN (United States)
Observed institutions:
National Aerospace Laboratories,
ViGYAN (United States)
OpenAlex ID:
A5035227610
Wing rock and roll attractor of delta wings at high angles of attack
1994
·
Bandu Pamadi
, Dhanvada Rao
, et al.
·
32nd Aerospace Sciences Meeting and Exhibit
·
25
Wind tunnel dynamic flying study of the pitching moment derivatives of the Standard Dynamics Model in active control
1987
·
S. BALAKRISHNA
, T. NIRANJANA
·
AIAA Atmospheric Flight Mechanics Conference
·
9
Estimation of aerodynamic derivatives using Dynamic Wind Tunnel Simulation Technique
1993
·
S. Balakrishna
, T Niranjana
, et al.
·
Institutional Repository @ NAL (University of Southampton)
·
6
A study of roll attractor and wing rock of delta wings at high angles of attack
1993
·
T Niranjana
, Dhanvada M. Rao
, et al.
·
NASA Technical Reports Server (NASA)
PDF
Estimation Of Longitudinal Moment Derivatives Of Missile Configuration Using Semi Free Flying Technique
1993
·
Rajamurthy
, Rajan
, et al.
·
Institutional Repository @ NAL (University of Southampton)
PDF
Recent contributions to system theoretic approach to flight mechanics research 13; 13;
1993
·
S. Srinathkumar
, Padma Madhuranath
, et al.
Estimation Of Roll Derivatives Of A 1/15 Scale LCA Model By Dynamic Wind Tunnel Simulation Technique
1992
·
S Srikanth kumar
, T Niranjana
, et al.
·
Institutional Repository @ NAL (University of Southampton)
PDF
A rotary derivative rig for FMCD low speed tunnel
1992
·
Balakrishna, S
, Niranjana, T
, et al.
·
Institutional Repository @ NAL (University of Southampton)
Augmentation of the 1.2m x 1.2m low speed dynamic test wind tunnel at NAL
1991
·
S. Balakrishna
, T Niranjana
, et al.
·
Institutional Repository @ NAL (University of Southampton)
Dynamic flying investigations on 1/13.5 NALLA Model (Longitudinal Results)
1991
·
S. Balakrishna
, T Niranjana
, et al.
·
Institutional Repository @ NAL (University of Southampton)
Flight data analysis of the short period characteristics of pushpak aircraft
1987
·
Padma Madhuranath
, T Niranjana
·
Institutional Repository @ NAL (University of Southampton)
Design and simulation of a Digital Combat Flap controller for a fighter Aircraft
1987
·
K. Karunakar
, NN Murthy
, et al.
·
Institutional Repository @ NAL (University of Southampton)
PDF
A Low Speed Tunnel Semi Free Dynamic Flying Study of Pitching Derivatives of LCA Delta-5 in Active Control using MLE Procedure
1987
·
S. Balakrishna
, T Niranjana
·
Institutional Repository @ NAL (University of Southampton)
PDF
Acoustic test facility system description manual
1986
·
S. Balakrishna
, VS Ganesh
, et al.
·
Institutional Repository @ NAL (University of Southampton)
Moment Stability Derivatives of Prithvi Missile Configurationat Low Speed Using Semi Free Dynamic Flying Method -Proposal
1986
·
S. Balakrishna
, T Niranjana
·
Institutional Repository @ NAL (University of Southampton)
A low speed tunnel semi-free dynamic flying study of the high angle of attack pitch derivatives of HF-24 using MILE procedure
1986
·
Balakrishna, S
, Niranjana, T
, et al.
·
Institutional Repository @ NAL (University of Southampton)
Ground based vehicle simulation - (Preliminary investigation)
1978
·
Padma Madhuranath
, Rajeswari P Ramamoorthy
, et al.
·
Institutional Repository @ NAL (University of Southampton)
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Works count:
18
Citation count:
40
H-index:
3
I10-index:
1
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