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Effect of nacelle orientation on the aerodynamic characteristics of an arrow wing-body configuration at Mach number 2.03Engine nacelle orientation effect on aerodynamic characteristics of arrow wing body configuration
Document ID
19660007273
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Landrum, E. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3284
Report Number: NASA-TN-D-3284
Accession Number
66N16562
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRCRAFT CONFIGURATION
WING BODY
ARROW WING
SUPERSONIC TRANSPORT
NACELLE
AERODYNAMIC CHARACTERISTICS
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