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Comparison of Tail and Wing-Tip Spin-Recovery Parachutes as Determined by Tests in the Langley 20-Foot Free-Spinning Tunnel
Document ID
19930092698
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Malvestuto, Frank S , Jr
Date Acquired
September 6, 2013
Publication Date
March 1, 1946
Report/Patent Number
NACA-ARR-L5G19A
NACA-WR-L-38
Report Number: NACA-ARR-L5G19A
Report Number: NACA-WR-L-38
Accession Number
93R21988
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SPINNING CHARACTERISTICS
WIND TUNNEL TESTS- NACA-FREE-SPINNING (20')
SPINNING- RECOVERY
PARACHUTES, AIRPLANE- TAIL
PARACHUTES, AIRPLANE- WING TIP
AIRPLANES, FIGHTER
SPINNING TESTS- NORTH AMERICAN BT-14 WIND TUNNEL (NACA-FREE-SPINNING-20')
AIRPLANES, TRAINING

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