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MACH 4.3 AND 4.4 SUPERSONIC WIND TUNNEL FLOW WITH SUPERSONIC SINGLE AND DUAL INJECTION

description

Summary

MACH 4.3 AND 4.4 SUPERSONIC WIND TUNNEL FLOW WITH SUPERSONIC SINGLE AND DUAL INJECTION

NASA Identifier: GRC-C-1998-959

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Tags

nasa mach 4 3 and 4 4 supersonic wind tunnel flow with supersonic single and dual injection dvids high resolution glenn research center aviation research organization
date_range

Date

1998
place

Location

create

Source

Defense Visual Information Distribution Service
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Link

https://www.dvidshub.net/
copyright

Copyright info

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

label_outline Explore Mach 4 3 And 4 4 Supersonic Wind Tunnel Flow With Supersonic Single And Dual Injection, Aviation Research Organization, Glenn Research Center

Topics

nasa mach 4 3 and 4 4 supersonic wind tunnel flow with supersonic single and dual injection dvids high resolution glenn research center aviation research organization