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Emergency Spin-Recovery Device for the 1/18-Scale Model of the Ryan X-13 Airplane as Determined from Tests in the Langley 20-Foot Free-Spinning TunnelAn investigation has been conducted in the Langley 20-foot free-spinning tunnel on a l/18-scale model of the Ryan X-13 airplane to determine the size parachute required for emergency-spin recovery during demonstration spins. Test results for erect spins indicate that a stable 12.73-foot-diameter parachute with a drag coefficient of 1.11 (based on the 12.73-foot projected diameter) is the minimum size required to insure satisfactory recovery in an emergency. The use of a stable parachute is recommended. Test results for inverted spins indicate that the l2.75-foot-diameter parachute is also satisfactory to terminate inverted spins.
Document ID
20050029375
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Bowman, James S., Jr.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 22, 2013
Publication Date
January 10, 1955
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-RM-SL55A25
Report Number: NACA-RM-SL55A25
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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