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Tests of Vortex-Ring Parachute at Supersonic Speed in the Langley Unitary Plan Wind TunnelFor the test, the 12-inch-diameter "Vortex-Ring" parachute was towed behind a conical-nosed cylindrical body 2.25 inches in diameter. The tow-cable length was 24 inches, and was attached to the cylindrical body through a large swivel and to the parachute through a smaller swivel. The attachment between the large swivel an the cylindrical body failed after about 1 minute's operation. Mach number was approximately 2.2, dynamic pressure was approximately 150 pounds per square foot, and camera speed was approximately 3000 frames per second.
Document ID
20070030947
Acquisition Source
Langley Research Center
Document Type
Video
Date Acquired
August 24, 2013
Publication Date
July 18, 1960
Subject Category
Aerodynamics
Report/Patent Number
L-560
Report Number: L-560
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC SPEED
RINGS
VORTEX RINGS
TESTS
[Division] UPWTD
[Tunnel] Langley Unitary Plan Wind Tunnel
WIND TUNNEL TESTS
VORTICES
PARACHUTES

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