Analysis and reduction of skin-friction in a rocket-based combined-cycle engine flow path operating from Mach 1.5 to 6.0-Reference-Cited by-同舟云学术

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Analysis and reduction of skin-friction in a rocket-based combined-cycle engine flow path operating from Mach 1.5 to 6.0

Published:2018-10 Issue: Volume:151 Page:357-367
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Wang Shuai,He Guo-qiang,Yan De-kun,Huang Zhi-wei^ORCID,Qin Fei^ORCID

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference45 articles.

1. The strutjet engine: exploding the myths surrounding high speed airbreathing propulsion;Bulman,1995

2. Recent progress in scramjet/combined cycle engines at JAXA Kakuda space center;Tetsuo;Acta Astronaut.,2006

3. Early studies of RBCC applications and lessons learned for today;Ehrlich,2000

4. Rocket based combined cycle hypersonic vehicle design for orbital access;Kothari,2011

5. Multi-objective, multidisciplinary design optimization of TSTO space planes with RBCC engines;Fujikawa,2015

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