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Devesh Kumar
Devesh Kumar
Boeing Research & Technology
Verified email at umich.edu
Title
Cited by
Cited by
Year
Buckling analysis of carbon nanotubes modeled using nonlocal continuum theories
D Kumar, C Heinrich, AM Waas
Journal of Applied Physics 103 (7), 073521, 2008
1282008
The AVINOR aeroelastic simulation code and its application to reduced vibration composite rotor blade design
B Glaz, P Friedmann, L Liu, D Kumar, C Cesnik
50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2009
322009
Design and Analysis of Composite Rotor Blades for Active/Passive Vibration Reduction
D Kumar
University of Michigan, 2013
172013
Rotordynamic Analysis using 3D elements in Fixed and Rotating Reference Frame
D Kumar
ASME 2016 International Mechanical Engineering Congress & Exposition (IMECE), 2016
102016
Performance Enhancement in Dynamic Stall Condition Using Active Camber Deformation
D Kumar, CES Cesnik
Journal of the American Helicopter Society 60 (2), 1-12, 2015
102015
Optimization Framework for Dynamic Analysis and Design of Active Twist Rotors
D Kumar, CES Cesnik, P Rohl, M Sutton
American Helicopter Society International 68th Annual Forum,, 2012
102012
Effect of Piezoceramic Actuator Hysteresis on Helicopter Vibration and Noise Reduction
ER Muir, L Liu, PP Friedmann, D Kumar
Journal of guidance, control, and dynamics 35 (4), 1299-1311, 2012
102012
New strategy for designing composite rotor blades with active flaps
D Kumar, CES Cesnik
Journal of Intelligent Material Systems and Structures 27 (9), 1176-1188, 2016
92016
New Optimization Strategy for Design of Active Twist Rotor
D Kumar, CES Cesnik
AIAA Journal 53 (2), 436-448, 2015
92015
IXGEN-A Modeling Tool for the Preliminary Design of Composite Rotor Blade
PJ Rohl, P Dorman, M Sutton, CES Cesnik, D Kumar
AHS future vertical lift design conference, 2012
92012
A Composite Rotor Blade Structural Design Environment for Aeromechanical Assessments in Conceptual and Preliminary Design
PJ Rohl, D Kumar, P Dorman, M Sutton, CES Cesnik
American Helicopter Society 68th Annual Forum and Technology Display, 2012
82012
A Multidisciplinary Design Environment for Composite Rotor Blades
PJ Rohl, P Dorman, M Sutton, D Kumar, CES Cesnik
53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Material …, 2012
8*2012
Determination of optimum camber distribution in rotating wings with deformable airfoils for vibration reduction and performance enhancement using surrogate modeling
D Kumar, B Glaz, J Mok, PP Friedmann, CES Cesnik
European Rotorcraft Forum, 2010
62010
Hysteresis Characterization in Piezoceramic Stack Actuators and Its Influence on Vibration and Noise Reduction in Helicopters Using Actively Controlled Flaps
E Muir, L Liu, P Friedmann, D Kumar
& Proceedings 저널· 프로시딩즈| 기술보고서| 해외연구초록| Reference DB| 공학 …, 2010
52010
Efficient Rotordynamic Analysis Using The Superelement Approach For An Aircraft Engine
D Kumar, K Juethner, Y Fournier
Proceedings of ASME Turbo Expo 2017: Turbomachinery Technical Conference and …, 2017
42017
Rapid Reconfiguration of Engines for Dynamics Simulation
D Kumar, K Juethner, Y Fournier
SAE 2016 Aerospace Systems and Technology Conference, 2016
42016
New Hybrid Optimization for Design of Active Twist Rotors
D Kumar, CE Cesnik
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2013
42013
High Fidelity Rotordynamic Analysis
D Kumar, PR Pamidi, H Patel
NAFEMS World Congress, San Diego, California June 21-24, 2015., 2015
32015
Force Measurements of a Flapping Wing with Two Angular Degrees of Freedom and Bio-Inspired Kinematics
CL Morrison, RBR Vandenheede, D Kumar, LP Bernal, C Cesnik
& Proceedings 저널· 프로시딩즈| 기술보고서| 해외연구초록| Reference DB| 공학 …, 2012
32012
Performance Enhancement and Vibration Reduction in Dynamic Stall Condition using Active Camber Deformation
D Kumar, CES Cesnik
American Helicopter Society 69th Annual Forum and Technology Display, 2013
2013
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Articles 1–20