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

1–12 von 12 Ergebnissen
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    Flowfield of an S-Shaped Inlet with High Boundary-Layer Ingestion Fraction

    Wang, Kun / Huang, He-xia / Liu, Lei et al. | AIAA | 2024
    Schlagwörter: Freestream Mach Number

    Characterization of Two Typical Unthrottled Flows in Hypersonic Inlet/Isolator Models

    Huang, He-xia / Sun, Shu / Tan, Hui-jun et al. | AIAA | 2015
    Schlagwörter: Mach Number

    Unthrottled Flows with Complex Background Waves in Curved Isolators

    Huang, He-xia / Tan, Hui-jun / Sun, Shu et al. | AIAA | 2017
    Schlagwörter: Freestream Mach Number

    Experiment of an Auxiliary Restart Method for Hypersonic Inlet with Variable-Bleed System

    Qin, Yuan / Huang, He-xia / Li, Fang-bo et al. | AIAA | 2023
    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

    Behavior of Shock Train in Curved Isolators with Complex Background Waves

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

    Morphing Supersonic Inlet with Deforming Air Cell

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

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

    Zhang, Yue / Tan, Hui-jun / Tian, Fang-Chao et al. | AIAA | 2014
    Schlagwörter: Freestream Mach Number

    Influence of Secondary Flow Injection Angle on a Fluidic Shock Control Technique

    Li, Cheng-hong / Tan, Hui-jun / Wang, De-peng | AIAA | 2015
    Schlagwörter: Freestream Mach Number

    Separated Flows in Bifurcated Region of a Vaneless Inertial Particle Separator

    Chen, Hao / Tan, Hui-jun / Yuan, Yong-qing et al. | AIAA | 2017
    Schlagwörter: Mach Number

    Influence of Expansion Waves on Cowl Shock/Boundary Layer Interaction in Hypersonic Inlets

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