Author:
Shu Sun,Hongying Zhang,Keming Cheng,Yizhao Wu
Subject
Mechanical Engineering,Aerospace Engineering
Reference14 articles.
1. Effects of airframe integrated configuration on scramjet inlet performance;Akihsa;AIAA,2000
2. Forebody compressibility research of hypersonic vehicle;Liu;Applied Mathematics and Mechanics,2004
3. Wind tunnel tests of hypersonic inlets for ramjet modules of ramjet-scramjet combined engine;Tan;Acta Aeronautica et Astronautica Sinica,2007
4. Kobyashi H, Sato T, Tanataugu N. Optimization of airbreathing propulsion system for the TSTO space-plane. AIAA 2001–1912, 2001.
5. Tsuchiya T, Mori T, Maita M. An integrated optimization for conceptual designs of airbreathing launch TSTO vehicle. AIAA 2001–1902, 2001.
Cited by
16 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献