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High Speed Schlieren Studies of Flow Over Mercury Atlas Vehicle in the Langley 2-Foot Transonic Aeroplasticity TunnelTest conditions for the studies are: Mach number varying continuously from approximately 0.8 to 1.1 and Reynolds number (based on maximum diameter of Atlas) approximately 0.451 x 10(exp 6). Camera speed is 2000 frames per second.
Document ID
20070030972
Acquisition Source
Langley Research Center
Document Type
Video
External Source(s)
http://lisar.larc.nasa.gov/MOVIES/LARGE/LV-2007-00017.mov
http://lisar.larc.nasa.gov/MOVIES/MEDIUM/LV-2007-00017.mov
Date Acquired
August 24, 2013
Publication Date
December 2, 1960
Subject Category
Aerodynamics
Report/Patent Number
L-583
Report Number: L-583
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
[Tunnel] 2-Foot Transonic Aeroplasticity Tunnel

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