Calspan's upgraded 96 inch hypersonic shock tunnel - Its development and application in the performance of research and testing at higher enthalpies-Reference-Cited by-同舟云学术

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Calspan's upgraded 96 inch hypersonic shock tunnel - Its development and application in the performance of research and testing at higher enthalpies

Published:1995-01-09 Issue: Volume: Page:
ISSN:
Container-title:33rd Aerospace Sciences Meeting and Exhibit
language:
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Author:

Albrechcinski T,Boyer D,Chadwick K,Lordi J

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-236

Reference10 articles.

1. EXPERIMENTALMEASUREMENTSWITH IDEALGASCALCULATION -1q -10 -16 -12 -8 -'i a ' i s ia is io a'i

2. u Po -2

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. The History of Hypersonic Research at Cornell Aeronautical Laboratory;AIAA SCITECH 2022 Forum;2022-01-03

2. On the Initial Characterization of a Large-Scale Hypervelocity Expansion Tunnel;AIAA SCITECH 2022 Forum;2022-01-03

3. Detonation-Driven Fuel-Injection System for Supersonic Combustion Testing Facilities;AIAA Journal;2018-08

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