A Design Concept for the Construction of a Complete Hypersonic Vehicle from 2D Flowfields-Reference-Cited by-同舟云学术

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A Design Concept for the Construction of a Complete Hypersonic Vehicle from 2D Flowfields

Published:2005-05-16 Issue: Volume: Page:
ISSN:
Container-title:AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference
language:
Short-container-title:

Author:

Ferguson Frederick¹,Zhang Shengyong¹,Apdin Hydar¹

Affiliation:

1. North Carolina A&T State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-3363

Reference14 articles.

1. Delta Wings of Shapes Amenable to Exact Shock-wave Theory

2. Delta Wings of Shapes Amenable to Exact Shock-wave Theory

3. 4Ferguson, F. "Expanding the Waverider Design Space Using Arbitrary Generating Flowfields", Ph.D. Dissertation, Department of Aerospace Engineering,Universityof Maryland,College Park, Maryland,1993

Cited by 3 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. Dual Waverider to Integrate External and Internal Flows;Journal of Aircraft;2020-05

2. Waverider Design and Analysis;20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2015-07-02

3. The Design, Analysis and Performance Evaluation of Waverider Configurations for Hypersonic Vehicle Applications;53rd AIAA Aerospace Sciences Meeting;2015-01-03

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