关注
Madhusudan A. Padmanabhan
Madhusudan A. Padmanabhan
Senior Scientist, Aeronautical Development Agency
在 gov.in 的电子邮件经过验证
标题
引用次数
引用次数
年份
Topology optimization of aircraft wing
JS Rao, S Kiran, JV Kamesh, MA Padmanabhan, S Chandra
Journal of Aerospace Sciences and Technologies, 402-414, 2009
332009
Store-induced limit-cycle oscillations due to nonlinear wing-store attachment
MA Padmanabhan, EH Dowell, JP Thomas, CL Pasiliao
Journal of Aircraft 53 (3), 778-789, 2016
202016
Computational study of aeroelastic limit cycles due to localized structural nonlinearities
MA Padmanabhan, EH Dowell, CL Pasiliao
Journal of Aircraft 55 (4), 1531-1541, 2018
172018
Simulation of aeroelastic limit-cycle oscillations of aircraft wings with stores
MA Padmanabhan, CL Pasiliao, EH Dowell
AIAA Journal 52 (10), 2291-2299, 2014
162014
Landing gear design/maintenance analysis for nonlinear shimmy
MA Padmanabhan, EH Dowell
Journal of Aircraft 52 (5), 1707-1710, 2015
152015
Calculation of aeroelastic limit cycles due to localized nonlinearity and static preload
MA Padmanabhan, EH Dowell
AIAA Journal 55 (8), 2762-2772, 2017
142017
Gust response computations with control surface freeplay using random input describing functions
MA Padmanabhan, EH Dowell
AIAA Journal 58 (7), 2899-2908, 2020
112020
Sliding wear and freeplay growth due to control surface limit cycle oscillations
MA Padmanabhan
Journal of Aircraft 56 (5), 1973-1979, 2019
82019
Computational study of aeroelastic response due to freeplay and flight loads
MA Padmanabhan, EH Dowell
AIAA Journal 59 (7), 2793-2799, 2021
72021
A statistics based method for mapping flight strains to loads
M Padmanabhan, K Nagesh, H Elattuvalappil
47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2006
52006
Study of nonlinear stiffness and damping effects on shimmy and flutter
MA Padmanabhan, EH Dowell
Journal of Aircraft 60 (6), 1976-1985, 2023
32023
A study of the active aeroelastic wing concept for a delta wing aircraft
S Das, K Venkatraman, MA Padmanabhan
AIAA Scitech 2021 Forum, 0730, 2021
12021
A Theoretical and Computational Study of Limit Cycle Oscillations in High Performance Aircraft
MA Padmanabhan
Duke University, 2015
12015
Schemes for active vibration control of plates
MA Padmanabhan
University of Maryland at College Park, 1995
11995
Aerostructural performance improvement in an unmanned long endurance aircraft using adaptive wing concept
AK Sampath, MA Padmanabhan, S Kattimani
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2023
2023
Roll performance of a flexible aircraft with active aeroelastic wing
AK Mayya, A Srivastava, MA Padmanabhan, K Venkatraman
AIAA SCITECH 2023 Forum, 1565, 2023
2023
An Approach to Aeroelastic Modeling and Simulation of Limit Cycle Oscillations of Aircraft Wings with Stores
MA Padmanabhan, CL Pasiliao, E Dowell
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2013
2013
Active Aeroelastic Wing Technology–A Preliminary Study
MA Padmanabhan
UNSTEADY RANS BASED IMPULSE RESPONSE STUDIES OF AGARD WING FOR AEROELASTIC AND FLUTTER ANALYSIS
SV Sajjan, MA Padmanabhan, S Mandal, G SenGupta, PK Dutta
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