search-head

You are here: Homepage >  Search

21–40 of 78 hits
|
Sort by:

    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

      Unsteady Aerostructure Coupled Adjoint Method for Flutter Suppression

      Zhang, Zhichao | Online Contents | 2015
      Contributors: Chen, P. C

    Adapted K-Method for Frequency-Domain ASE Control Stability Margin Analysis (AIAA 2014-1198)

    Wang, Z. / Chen, P.-C. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2014

    Unsteady subsonic aerodynamics for bodies and wings with external stores including wake effect

    CHEN, P. C. / LEE, H. W. / LIU, D. D. | AIAA | 1993

    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

    Free vibration solution for clamped orthotropic plates using Lagrangian multiplier technique

    RAMKUMAR, R. L. / CHEN, P. C. / SANDERS, W. J. | AIAA | 1987

    Development of a fluid driven rotor based on differential temperature

    Chen, P.-C. / Chang, S.-M. / Chiang, C.-H. et al. | TIBKAT | 2018

    Investigation of the Prediction Error Identification for Flutter Prediction

    Zeng, J. / Chen, P.-C. / Kukreja, S. et al. | British Library Conference Proceedings | 2012

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

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

    Unsteady supersonic flow calculations for wing-body combinations using harmonic gradient method

    GARCIA-FOGEDA, PABLO / LIU, D. D. / CHEN, P. C. | AIAA | 1990

    Robust gain-scheduled control for vertical/short take-off and landing aircraft in hovering with time-varying mass and moment of inertia

    Wu, S-L / Chen, P-C / Chang, K-Y et al. | SAGE Publications | 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

    Oscillating wings and bodies with flexure in supersonic flow

    LIU, D. D. / GARCIA-FOGEDA, P. / CHEN,P. C. | AIAA | 1988

    The State-of-the-Art of Unsteady Aerodynamics for High Performance Aircraft

    Yurkovich, R. N. / Liu, D. D. / Chen, P. C. et al. | British Library Conference Proceedings | 2001

    Store Separation Analysis at Subsonic and Supersonic Speeds using A High-Order

    Chen, P. C. / Advisory Group for Aerospace Research & Development | British Library Conference Proceedings | 1996

Number of results
10 50

Filter search results