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Some interference effects that influence vertical-tail loads at supersonic speedsAerodynamic interference effects on effectiveness of aircraft vertical tail at supersonic speeds
Document ID
19660010448
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Edwards, S. S. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
February 17, 1956
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-A55H30
Report Number: NACA-RM-A55H30
Accession Number
66N19737
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY AND CONTROL
SUPERSONIC FLIGHT
VERTICAL FIN
AERODYNAMIC CHARACTERISTICS
AIRCRAFT DESIGN

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