1–10 von 10 Ergebnissen
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    Endothermic Heat-Sink of Jet Fuels for Scramjet Cooling

    Huang, He / Spadaccini, Louis / Sobel, David | AIAA | 2002

    Unified Modeling Method for Large Space Structures Using Absolute Nodal Coordinate

    Li, Qingjun / Deng, Zichen / Zhang, Kai et al. | AIAA | 2018

    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

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

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

    Flowfield of an S-Shaped Inlet with High Boundary-Layer Ingestion Fraction

    Wang, Kun / Huang, He-xia / Liu, Lei et al. | AIAA | 2024

    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

    Fuel Composition Influence on Deposition from Endothermic Fuels

    Edwards, Tim / DeWitt, Matthew / Shafer, L. et al. | AIAA | 2006