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Aerodynamic characteristics in pitch, including effects of horizontal-tail negative dihedral angle, of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speedsAerodynamic characteristics in pitch of horizontal attitude VTOL aircraft, including effects of negative dihedral horizontal tail
Document ID
19660011610
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
December 1, 1960
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-11
Report Number: NASA-TM-X-11
Accession Number
66N20899
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PITCHING MOMENT
HORIZONTAL ATTITUDE
AERODYNAMIC CHARACTERISTICS
TAIL SURFACE

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