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Flight tests of a rotating cylinder flap on a North American Rockwell YOV-10 aircraftFlight tests were conducted of a twin engine airplane modified to a STOL configuration with rotating cylinder flaps and interconnected propellers. The flight tests included verification of the functional operation of the rotating cylinder flap system and the determination of the low speed flying qualities and performance characteristics with emphasis on approach and landing.
Document ID
19730004293
Document Type
Contractor Report (CR)
Authors
Cichy, D. R. (North American Rockwell Corp. Columbus, OH, United States)
Harris, J. W. (North American Rockwell Corp. Columbus, OH, United States)
Mackay, J. K. (North American Rockwell Corp. Columbus, OH, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1972
Subject Category
AIRCRAFT
Report/Patent Number
NASA-CR-2135
Funding Number(s)
CONTRACT_GRANT: NAS2-5326
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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NameType 19730004293.pdf STI