1–10 von 10 Ergebnissen
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    Variable geometry cowl sidewall for improving rectangular hypersonic inlet performance

    Teng, Jian / Yuan, Huacheng | Elsevier | 2015

      Variable geometry cowl sidewall for improving rectangular hypersonic inlet performance

      Teng, Jian | Online Contents | 2015
      Beteiligte: Yuan, Huacheng

    Turbine Based Combined Cycle Inlet Mode Transition at Different Operation Conditions (AIAA 2017-2118)

    Liu, Jun / Yuan, Huacheng / Ge, Ning | British Library Conference Proceedings | 2017

    Experimental and Numerical Research on a Three-Dimensional Inward-Turning Inlet

    Yuan, Huacheng / Li, Zheng / Zhang, Jinsheng et al. | ASCE | 2023

    Experimental and numerical investigation of a supersonic inlet with double S-bend diffuser

    Zhang, Jinsheng / Yuan, Huacheng / Wang, Yunfei et al. | SAGE Publications | 2021

    Aerodynamic design and performance analysis of a two-dimensional variable geometry inlet

    Yuan, Huacheng / Wang, Yunfei / Liu, Jun et al. | AIAA | 2017

    Aerodynamic Design and Performance Analysis of a Two-dimensional Variable Geometry Inlet (AIAA 2017-2275)

    Yuan, Huacheng / Wang, Yunfei / Liu, Jun et al. | British Library Conference Proceedings | 2017

    Design and Research of a Wave-rider Inlet Based on a Curved Shock under a Hypersonic Lift-body (AIAA 2017-2418)

    Yu, Anyuan / Yang, Dawei / Wang, Tiejun et al. | British Library Conference Proceedings | 2017

    Experimental and numerical investigation of smooth turbine-based combined-cycle inlet mode transition

    Liu, Jun | Online Contents | 2016
    Beteiligte: Yuan, Huacheng