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Transonic wind-tunnel investigation of the effect of control span and large wing-tip nacelles on effectiveness of spoiler-slot- deflector controls on an unswept-wing fighter-type airplaneTransonic wind tunnel study of control span and large wing-tip nacelles results on effectiveness of spoiler-slot-deflector controls on fighter aircraft
Document ID
19660012274
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Wornom, D. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1960
Subject Category
Biotechnology
Report/Patent Number
NASA-TM-X-280
Accession Number
66N21563
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL
CONTROL SURFACE
AIRCRAFT CONTROL
NACELLE

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