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AERODYNAMIC CHARACTERISTICS OF TWO RECTANGULAR-PLAN-FORM, ALLMOVABLE CONTROLS IN COMBINATION WITH A SLENDER BODY OF REVOLUTION AT MACH NUMBERS FROM 3.00 TO 6.25Aerodynamic characteristics of rectangular planform, all-movable controls combined with slender body of revolution at mach 3 to 6.25
Document ID
19630003238
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Gloria, H. R. (NASA Ames Research Center Moffett Field, CA, United States)
Wong, T. J. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 1, 2013
Publication Date
December 28, 1955
Subject Category
Auxiliary Systems
Report/Patent Number
NACA-RM-A55J07
Report Number: NACA-RM-A55J07
Accession Number
63N13114
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SLENDER BODY
RECTANGULAR PLANFORM
AERODYNAMIC CHARACTERISTICS
CONTROL SURFACE
BODY OF REVOLUTION

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