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-Prus June 6, 2024

Fuzhou LIU, Huacheng YUAN, Keyu ZHOU, Zhenggui ZHOU

DOI Number: https://doi.org/10.82241/ceas-hisst-2024-315

Conference number: HiSST-2024-315

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-Prus May 9, 2024

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

DOI Number: N/A

Conference number: HiSST-2024-037

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

HiSST 2018, Hypersonic Flight Dynamics, Hypersonic Propulsion, Propulsion Systems and ComponentsBy tvermin October 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 tvermin October 6, 2023

Jialin Zheng and Daren Yu

DOI Number XXX-YYY-ZZZ

Conference Number HiSST 2018-0809