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Wind-tunnel Investigation of Drag and Stability of Parachutes at Supersonic SpeedsWind tunnel investigation of drag and stability characteristics of flat roof conical inlet parachute
Document ID
19650020588
Document Type
Technical Memorandum (TM)
Authors
Charczenko, N. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1964
Subject Category
AERODYNAMICS
Report/Patent Number
NASA-TM-X-991
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PARACHUTE
FLAT SURFACE
CONICAL INLET
WIND TUNNEL

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