1–8 von 8 Ergebnissen
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    An Estimation Method for Scramjet Inlet Mach Number and Mass Flow Rate Based on Deep Learning

    Kong, Chen / Liu, Hao / Xu, Cheng et al. | Springer Verlag | 2022

    Micro-Ramp Control for Shock Train Structure and Oscillation

    Wang, Ziao / Chang, Juntao / Kong, Chen et al. | AIAA | 2021

    Flowfield Reconstruction and Shock Train Leading Edge Detection in Scramjet Isolators

    Kong, Chen / Chang, Juntao / Li, Yunfei et al. | AIAA | 2020

    Prediction model of temperature field in dual-mode combustors based on wall pressure

    Kong, Chen / Quan, Fuxu / Li, Yunfei et al. | Elsevier | 2022

    Efficient Prediction of Supersonic Flowfield in an Isolator Based on Pressure Sequence

    Kong, Chen / Zhang, Chenlin / Wang, Ziao et al. | AIAA | 2021

    Mechanism of shock-train/boundary-layer interaction in spanwise concave isolator channels

    Wang, Ziao / Xin, Xuanan / Huang, Renzhe et al. | Elsevier | 2022

    Development and evolution mechanism of streamwise vortex in an inward-turning inlet

    Wang, Ziao / Xin, Xuanan / Chen, Ruoyu et al. | SAGE Publications | 2023