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Effects of three spanwise twist variations on the longitudinal aerodynamic characteristics of a thin 45 deg sweptback highly tapered wing at transonic speedsDetermination of loads due to wing twist at transonic and low supersonic speeds
Document ID
19650003091
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mugler, J. P., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1959
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-126
Report Number: NASA-TM-X-126
Accession Number
65N12692
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING
TRANSONIC SPEED
LOAD TEST
SUPERSONIC SPEED

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