Buckling analysis of carbon nanotubes modeled using nonlocal continuum theories D Kumar, C Heinrich, AM Waas Journal of applied physics 103 (7), 2008 | 135 | 2008 |
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 | 33 | 2009 |
Design and Analysis of Composite Rotor Blades for Active/Passive Vibration Reduction D Kumar University of Michigan, 2013 | 21 | 2013 |
Rotordynamic Analysis using 3D elements in Fixed and Rotating Reference Frame D Kumar ASME 2016 International Mechanical Engineering Congress & Exposition (IMECE), 2016 | 14 | 2016 |
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 | 12 | 2012 |
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 | 11 | 2016 |
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 | 11 | 2015 |
IXGEN—A Modeling Tool for the Preliminary Design of Composite Rotor Blades PJ Rohl, P Dorman, CES Cesnik, D Kumar American Helicopter Society Future Vertical Lift Aircraft Design Conference …, 2012 | 11 | 2012 |
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 | 10 | 2012 |
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 | 10 | 2012 |
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 | 9 | 2017 |
New Optimization Strategy for Design of Active Twist Rotor D Kumar, CES Cesnik AIAA Journal 53 (2), 436-448, 2015 | 9 | 2015 |
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 | 9* | 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 | 7 | 2010 |
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 | 5 | 2010 |
Rapid Reconfiguration of Engines for Dynamics Simulation D Kumar, K Juethner, Y Fournier SAE 2016 Aerospace Systems and Technology Conference, 2016 | 4 | 2016 |
High Fidelity Rotordynamic Analysis D Kumar, PR Pamidi, H Patel NAFEMS World Congress, San Diego, California June 21-24, 2015., 2015 | 4 | 2015 |
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 | 4 | 2013 |
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 | 3 | 2012 |
Flutter Analysis of a Twin-Engine Airplane Using FUN3D-LFD D Kumar, M Hong, A Scalabrin, S Ruegamer AIAA SCITECH 2025 Forum, 0820, 2025 | | 2025 |