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DUCT LAB SUPERSONIC WIND TUNNEL MACH 4.3 PLUS FLOW WITH AND WITHOUT DUAL AIR INJECTION

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Summary

DUCT LAB SUPERSONIC WIND TUNNEL MACH 4.3 PLUS FLOW WITH AND WITHOUT DUAL AIR INJECTION

NASA Identifier: C-1998-492

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nasa duct lab supersonic wind tunnel mach 4 3 plus flow with and without dual air injection dvids high resolution glenn research center aviation research organization wind tunnel engineering
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Date

1998
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Defense Visual Information Distribution Service
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Link

https://www.dvidshub.net/
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Public Domain Dedication. Public Use Notice of Limitations: https://www.dvidshub.net/about/copyright

label_outline Explore Duct Lab Supersonic Wind Tunnel Mach 4 3 Plus Flow With And Without Dual Air Injection, Wind Tunnel, Engineering

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nasa duct lab supersonic wind tunnel mach 4 3 plus flow with and without dual air injection dvids high resolution glenn research center aviation research organization wind tunnel engineering