Synonyme wurden verwendet für: Mach-Zahl
Suche ohne Synonyme: keywords:("Mach-Zahl")

1–10 von 12 Ergebnissen
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    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
    Schlagwörter: Freestream Mach Number

    Ramp Shock Regulation of Supersonic Inlet with Shape Memory Alloy Plate

    Zhang, Yue / Tan, Hui-Jun / Li, Jie-Feng et al. | AIAA | 2018
    Schlagwörter: Freestream Mach Number

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

    Chen, Hao / Tan, Hui-Jun / Zhang, Qi-Fan et al. | AIAA | 2017
    Schlagwörter: Freestream Mach Number

    Experimental and Numerical Investigation of a Fluidically Variable Hypersonic Inlet

    Zhang, Yue / Tan, Hui-Jun / Sun, Shu et al. | AIAA | 2017
    Schlagwörter: Freestream Mach Number

    Oscillations in Rectangular Supersonic Inlets with Large Internal Contraction Ratio

    Jin, Yi / Zhang, Yue / Tan, Hui-Jun et al. | AIAA | 2022
    Schlagwörter: Freestream Mach Number

    Shock Control Method for Hypersonic Inlets Based on Forebody Secondary Flow Recirculation

    Zhang, Yue / Tan, Hui-Jun / Chen, Hao et al. | AIAA | 2018
    Schlagwörter: Freestream Mach Number

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

    Zhang, Yue / Tan, Hui-jun / Sun, Shu et al. | AIAA | 2015
    Schlagwörter: Freestream Mach Number

    Throttling Characteristics of a Supersonic Variable Inlet at Different Internal Contraction Ratios

    Jin, Yi / Sun, Shu / Zhang, Yue et al. | AIAA | 2022
    Schlagwörter: Freestream Mach Number

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

    Chen, Hao / Tan, Hui-Jun / Zhang, Qi-Fan et al. | AIAA | 2018
    Schlagwörter: Freestream Mach Number

    Morphing Supersonic Inlet with Deforming Air Cell

    Zhang, Yue / Tan, Hui-jun / Zhuang, Yi et al. | AIAA | 2014
    Schlagwörter: Freestream Mach Number