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Large-scale wind-tunnel tests of a propeller-driven deflected slipstream STOL model in ground effectWind tunnel tests of propellor driven, deflected slipstream, short takeoff aircraft model to determine longitudinal and lateral-directional stability when in ground effect
Document ID
19710026960
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Page, V. R. (NASA Ames Research Center Moffett Field, CA, United States)
Aiken, T. N. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1971
Subject Category
Aircraft
Report/Patent Number
A-3927
NASA-TM-X-2313
Report Number: A-3927
Report Number: NASA-TM-X-2313
Accession Number
71N36436
Funding Number(s)
PROJECT: RTOP 721-60-10-05-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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