visibility Similar

code Related

MACH 4.3 SUPERSONIC WIND TUNNEL FLOW WITH DUAL SUPERSONIC AND / OR SINGLE FLOOR INJECTION USING POSITIVE 50 DIOPTER SHADOWGRAPH SYSTEM CORRECTION

description

Summary

MACH 4.3 SUPERSONIC WIND TUNNEL FLOW WITH DUAL SUPERSONIC AND / OR SINGLE FLOOR INJECTION USING POSITIVE 50 DIOPTER SHADOWGRAPH SYSTEM CORRECTION

NASA Identifier: C-1998-1283

Nothing Found.

label_outline

Tags

nasa mach 4 3 supersonic wind tunnel flow with dual supersonic and or single floor injection using positive 50 diopter shadowgraph system correction dvids high resolution glenn research center aviation research organization wind tunnel engineering
date_range

Date

1998
place

Location

create

Source

Defense Visual Information Distribution Service
link

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 Supersonic Wind Tunnel Flow With Dual Supersonic And Or Single Floor Injection Using Positive 50 Diopter Shadowgraph System Correction, Wind Tunnel, Engineering

Topics

nasa mach 4 3 supersonic wind tunnel flow with dual supersonic and or single floor injection using positive 50 diopter shadowgraph system correction dvids high resolution glenn research center aviation research organization wind tunnel engineering