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The effects of wing-tip droop on the aerodynamic characteristics of a delta-wing aircraft at supersonic speedsWing-tip droop effects on performance and stability of canard delta-wing aircraft at supersonic speeds
Document ID
19660010439
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Petersen, R. H. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1960
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-363
Report Number: NASA-TM-X-363
Accession Number
66N19728
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC FLIGHT
AIRCRAFT DESIGN
AERODYNAMIC CHARACTERISTICS
WING TIP
DELTA WING

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