1–20 von 52 Ergebnissen
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    Influence of Secondary Flow Injection Angle on a Fluidic Shock Control Technique

    Li, Cheng-hong / Tan, Hui-jun / Wang, De-peng | AIAA | 2015

    Throttling Process and Buzz Mechanism of a Supersonic Inlet at Overspeed Mode

    Chen, Hao / Tan, Hui-Jun / Zhang, Qi-Fan et al. | AIAA | 2018

    Control of Cowl-Shock/Boundary-Layer Interactions by Deformable Shape-Memory Alloy Bump

    Zhang, Yue / Tan, Hui-Jun / Li, Jie-Feng et al. | AIAA | 2018

    Buzz Flows in an External-Compression Inlet with Partially Isentropic Compression

    Chen, Hao / Tan, Hui-Jun / Zhang, Qi-Fan et al. | AIAA | 2017

    Control of Cowl Shock/Boundary-Layer Interaction in Hypersonic Inlets by Bump

    Zhang, Yue / Tan, Hui-jun / Sun, Shu et al. | AIAA | 2015

    External-Compression Supersonic Inlet Free from Violent Buzz

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

    Control of Incident Shock/Boundary-Layer Interaction by a Two-Dimensional Bump

    Zhang, Yue / Tan, Hui-jun / Tian, Fang-Chao et al. | AIAA | 2014

    Morphing Supersonic Inlet with Deforming Air Cell

    Zhang, Yue / Tan, Hui-jun / Zhuang, Yi et al. | AIAA | 2014

    Behavior of Shock Train in Curved Isolators with Complex Background Waves

    Huang, He-xia / Tan, Hui-jun / Sun, Shu et al. | AIAA | 2017

    Unthrottled Flows with Complex Background Waves in Curved Isolators

    Huang, He-xia / Tan, Hui-jun / Sun, Shu et al. | AIAA | 2017