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Schlieren Movies of the 8-Inch Diameter Rigid Parachute Model of the Cook Research Laboratory Taken During the Fourth Phase of Testing in the Langley Unitary Plan Wind TunnelCanopy Model IV was tested in four different configuration series. Shroud lines were used in the first three series of tests; none were used in the fourth series. Other variables were Mach number (1.77, 2.17, 2.76), dynamic pressure (290, 250, 155 lb per sq ft), camera speed, and attitude.
Document ID
20070030956
Acquisition Source
Langley Research Center
Document Type
Video
Date Acquired
August 24, 2013
Publication Date
September 29, 1958
Subject Category
Aerodynamics
Report/Patent Number
L-396
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
[Tunnel] Unitary Plan Wind Tunnel

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