Experimental and numerical study on reinforcement mechanism of embedded rocket on back pressure resistance of RBCC inlet at starting stage-Reference-Cited by-同舟云学术

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Experimental and numerical study on reinforcement mechanism of embedded rocket on back pressure resistance of RBCC inlet at starting stage

Published:2022-04 Issue: Volume:123 Page:107487
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Shi Lei^ORCID,Yang Yiyan^ORCID,Yang Xue,Ran Rui^ORCID,Qin Fei,He Guoqiang

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

1. Research progress on ejector mode of rocket-based combined-cycle engines;Shi;Prog. Aerosp. Sci.,2019

2. T. Fujikawa, T. Tsuchiya, S. Tomioka, Multi-objective, multidisciplinary design optimization of TSTO space planes with RBCC engines, AIAA Paper 2015-0650.

3. Recent research progress on unstart mechanism, detection and control of hypersonic inlet;Chang;Prog. Aerosp. Sci.,2017

4. Scramjet inlets;Van;Scramjet Propuls.,2000

5. D.M. Van Wie, F.T. Kwok, R.F. Walsh, Starting characteristics of supersonic inlets, AIAA Paper 1996–2914.

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