Stagnation Temperature Measurements for Hypersonic Intake Testing in a Gun Tunnel Flow-Reference-Cited by-同舟云学术

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Stagnation Temperature Measurements for Hypersonic Intake Testing in a Gun Tunnel Flow

Published:2006-06-15 Issue: Volume: Page:
ISSN:
Container-title:14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference
language:
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Author:

Matthews Alexander¹,Munro Stuart¹,Sweeney William¹

Affiliation:

1. University of Oxford

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-8107

Reference19 articles.

1. A gun tunnel investigation of hypersonic free shear layers in a planar duct

2. Performance and Operability of an Isentropic-Spike Intake with Annular Isolator Sections

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. Performance and Operability of an Isentropic-Spike Intake with Annular Isolator Sections;14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference;2006-06-15

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