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FREE-FLIGHT INVESTIGATION AT TRANSONIC SPEEDS OF THE STABILITY CHARACTERISTICS OF A TAILLESS MISSILE CONFIGURATION HAVING A 45 DEG SWEPTBACK WING OF ASPECT RATIO 4Free flight test of tailless missile configuration with 45-deg sweptback wing of aspect ratio 4 - stability at transonic speeds
Document ID
19630004110
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Arbic, R. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 1, 2013
Publication Date
August 28, 1956
Subject Category
Space Sciences
Report/Patent Number
NACA-RM-L56E11
Accession Number
63N13986
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRANSONIC SPEED
MISSILE CONFIGURATION
AERODYNAMIC STABILITY
TAILLESS AIRCRAFT
SWEPTBACK WING

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