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Chen, P. C.   Clear all
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    Design-Oriented Computational Fluid Dynamics-Based Unsteady Aerodynamics for Flight-Vehicle Aeroelastic Shape Optimization

    Chen, P. C. / Zhang, Zhichao / Livne, Eli | AIAA | 2015

    Nonlinear Aeroelastic Studies on a Folding Wing Configuration with Free-Play Hinge Nonlinearity

    Lee, Dong Hwan / Chen, P. C. | AIAA | 2006

    Nonlinear Flutter Analysis for the Scaled F-35 with Horizontal-Tail Free Play

    Chen, P. C. / Ritz, Erich / Lindsley, Ned | AIAA | 2014

    Nonlinear Aeroelastic Studies on a Joined-Wing with Wing Buckling Effects

    Lee, Dong-Hwan / Chen, P. C. | AIAA | 2004

    Studies of Aerodynamic Influence of Under-Wing Stores on Flutter Characteristics of F-16

    Lee, Dong-Hwan / Chen, P. C. | AIAA | 2009

    CFD-Based Control for Flutter Suppression, Gust Load Alleviation, and Ride Quality Enhancement for the S4T Model

    Moulin, Boris / Ritz, Erich / Chen, P. C. et al. | AIAA | 2010

    Reduced-Order Nonlinear Damping Model: Formulation and Application to Postflutter Aeroelastic Behavior

    Wang, X. Q. / Song, Pengchao / Mignolet, Marc P. et al. | AIAA | 2021

    Nonlinear Aeroelastic Analysis for A HALE Wing Including Effects of Gust and Flow Separation

    Wang, Zhicun / Chen, P. C. / Liu, Danny et al. | AIAA | 2007

    Extension of the g-Method Flutter Solution to Aeroservoelastic Stability Analysis

    Karpel, Moti / Moulin, Boris / Chen, P. C. | AIAA | 2003

    Versatile Controller For CCD's

    Novello, J. / Chen, P. C. | NTRS | 1994

    Impact of Aerodynamic and Structural Parameters on Control Surface Buzz

    Pai, Fang-Ping / Yang, Lee-Jang / Huang, Ying-Hsuan et al. | AIAA | 2021

    Graphite fiber strengthens lightweight mirrors Composites based on graphite fibers allow large-aperture mirrors to be made extremely lightweight, while maintaining rigidity and strength

    Chen, P. C. / Romeo, R. C. | British Library Online Contents | 2001

    Unsteady Aerostructure Coupled Adjoint Method for Flutter Suppression

    Zhang, Zhichao / Chen, P. C. / Yang, Shuchi et al. | AIAA | 2015

    Hybrid Optimization Framework with Proper-Orthogonal-Decomposition-Based Order Reduction and Design-Space Evolution Scheme

    Ghoman, Satyajit S. / Wang, Zhicun / Chen, P. C. et al. | AIAA | 2013

    LIMIT CYCLE OSCILLATON PREDICTION FOR AIRCRAFT WITH EXTERNAL STORES — IFASD 2019

    Chen, P. C. / Zhang, Z. / Zhou, Z. et al. | TIBKAT | 2020

    Modeling-Based Hyper-Reduction of Multidimensional Computational Fluid Dynamics Data: Application to Ship Airwake Data

    Wang, X. Q. / Sarhaddi, D. / Wang, Z. et al. | AIAA | 2019

    CFD-Based Aeroservoelastic Control for Supersonic Flutter Suppression, Gust Load Alleviation, and Ride Quality Enhancement

    Chen, P. C. / Moulin, Boris / Ritz, Erich et al. | AIAA | 2009

    Flutter Analysis with Structural Uncertainty by Using CFD-Based Aerodynamic ROM

    Wang, Zhicun / Zhang, Zhichao / Lee, D. H. et al. | AIAA | 2008

    Time Domain Nonlinear Aeroelastic Analysis for HALE Wings

    Wang, Zhicun / Chen, P. C. / Liu, D. D. et al. | AIAA | 2006

    Focal length calibration from two views: method and analysis of singular cases

    Sturm, P. / Cheng, Z. L. / Chen, P. C. et al. | British Library Online Contents | 2005

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