1–18 von 18 Ergebnissen
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    Control of Pressure Oscillations Induced by Supersonic Cavity Flow

    Xiansheng, Wang / Dangguo, Yang / Jun, Liu et al. | AIAA | 2020

    Design Under Uncertainty Using a Combination of Evidence Theory and a Bayesian Approach

    Zhou, Jun / Ellis, Clifton / Mourelatos, Zissimos P. | AIAA | 2008

    External-Compression Supersonic Inlet Free from Violent Buzz

    Chen, Hao / Tan, Hui-jun / Liu, Ya-zhou et al. | AIAA | 2019

    Fuzzy logic based hovering control system design

    Ammeen, Edward / Zhou, Zhiqing / Yu, Tie-Jun et al. | AIAA | 1997

    Helicopter Rotor Performance Improvement with Multidisciplinary Aerodynamic Optimization

    Xie, Jiayi / Xie, Zhifeng / Zhou, Ming et al. | AIAA | 2017

    Integrated model and matching control of turbo shaft triple engines with helicopter rotor

    Shi, Rui-jun / Zhou, Jian-bo / Zhang, Qiu-gui et al. | AIAA | 2017

    ObjecTime modeling, animation and architecture of fire control

    Coleman, Norm / May, Ricky / Yip, Pak et al. | AIAA | 1998

    Sound generation by different vortex interactions in mixing layers

    Zhou, Lin / Wan, Zhenhua / Sun, De-Jun et al. | AIAA | 2012

    Stall-Warning Approach Based on Aeroacoustic Principle

    Li, Fanyu / Li, Jun / Dong, Xu et al. | AIAA | 2016

    The Attitude Control of Small Spacecraft with Movable Appendage

    Han, Congying / Guo, Jian / You, Zheng et al. | AIAA | 2003