A Computational Investigation of Flow Through an Axisymmetric Supersonic Inlet-Reference-Cited by-同舟云学术

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A Computational Investigation of Flow Through an Axisymmetric Supersonic Inlet

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
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Author:

Conway Matthew¹,Lavely Adam¹,Blaisdell Gregory¹

Affiliation:

1. Purdue University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-941

Reference14 articles.

1. A Summary of Recent Supersonic Vehicle Studies at Gulfstream Aerospace

2. Supersonic Inlet Shaping for Dramatic Reductions in Drag and Sonic Boom Strength

3. Dynamic Analysis of Wind Tunnel Data from an Isentropic Relaxed Compression Inlet

4. CFD Results for an Axisymmetric Isentropic Relaxed Compression Inlet

Cited by 2 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. A Flow Simulation of an Axisymmetric Supersonic Inlet with Support Struts and Annular Bypass Duct;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

2. Effects of Radial Distortion on Performance of a Fan;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

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