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Effects of vertical-tail size and a ventral fin on the static lateral and directional stability derivatives of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speedsVertical tail size and ventral fin effects on lateral and directional stability of VTOL AIRCRAFT at transonic speeds
Document ID
19660010786
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Olstad, W. B. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1960
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-35
Accession Number
66N20075
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VTOL AIRCRAFT
DIRECTIONAL STABILITY
VERTICAL TAIL
TRANSONIC SPEED
LATERAL STABILITY

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