Airframe-Propulsion Integration Methodology for Waverider-Derived Hypersonic Cruise Aircraft Design Concepts-Reference-Cited by-同舟云学术

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Airframe-Propulsion Integration Methodology for Waverider-Derived Hypersonic Cruise Aircraft Design Concepts

Published:2004-01-05 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Javaid Kashif¹,Serghides Varnavas¹

Affiliation:

1. Imperial College London

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-1201

Reference18 articles.

1. 1Bowcutt, K., Jr., J. A., and Capriotti, D. “Viscous Optimized Hypersonic Waveriders,” Tech. Rep. AIAA 87-0272, 1987.

2. 4Carreiro, L. “PDWAP: A preliminary design and weights analysis program for aerospace vehicles,” Tech. Rep. AD-A222614, Jan 1990.

3. Analysis of a hypersonic waverider research vehicle with a hydrocarbon scramjet engine

Cited by 1 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

1. Novel inlet–airframe integration methodology for hypersonic waverider vehicles;Acta Astronautica;2015-06

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