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Unitary Wind Tunnel Tests of 30-Degree Conical Ribbon Parachute and a Rotofoil Parachute Towed in the Wake of a Conical Nosed Cylindrical BodyMultiple wind tunnel test trials were conducted on a 30 degree conical ribbon parachute with porosities of 30, 27, and 24 percent. Variables were Mach number, dynamic pressure, towline length, and coefficient of drag. A Rotofoil parachute having a porosity of approximately 24 percent was tested, but failed after about 30 seconds of operation at a Mach number of 1.8 All of the parachutes had a nominal diameter and shroud line length of 10 inches. Drag coefficients were based on the area of a circle having a diameter two-thirds of the nominal parachute diameter.
Document ID
20070030965
Acquisition Source
Langley Research Center
Document Type
Video
Date Acquired
August 24, 2013
Publication Date
March 2, 1962
Subject Category
Aerodynamics
Report/Patent Number
L-683
Report Number: L-683
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL TESTS
EXPERIMENTS
[Division] Unitary Planned Wind Tunnel
TESTS

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