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Tag Archives: TBCC

Design and Starting Study of the Adjustable Inward Turning Inlet at Ma1.5~7

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-PrusJune 6, 2024

Fuzhou LIU, Huacheng YUAN, Keyu ZHOU, Zhenggui ZHOU

DOI Number: 10.60853/39s2-kn63

Conference number: HiSST-2024-00315

Experimental and Numerical Research on a Design Concept of Two-stage Compression Inward-turning TBCC Inlet

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-PrusMay 9, 2024

Zhancang HU, Yiqi TANG, Zhonglong LI, Zejun CAI, Zhenqi SUN, Chengxiang ZHU, Yancheng YOU

DOI Number: XXX-YYY-ZZZ

Conference number: HiSST 2024 – 0037

Design and Numerical Simulation of a Common Nozzle of multi-Channel TBCC Engine

HiSST 2018, Hypersonic Flight Dynamics, Hypersonic Propulsion, Propulsion Systems and ComponentsBy tverminOctober 26, 2023

Rongqian Chen  , Yangcan Huang  , Chengxiang Zhu , Ruofan Qiu  , Yancheng You

DoI Number XXX-YYY-ZZZ

Conference Number HiSST 2018_41601152

Design of Gravity-Assist Trajectories for Thrust Pinch in an Integrated Aircraft-Propulsion System

HiSST 2018, Hypersonic Aerodynamics, Hypersonic Propulsion, Operations and Environment, Propulsion Systems and ComponentsBy tverminOctober 6, 2023

Jialin Zheng  and Daren Yu

DOI Number XXX-YYY-ZZZ

Conference Number HiSST 2018-0809

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