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DESIGN CONCEPTS FOR MINIMUM WEIGHT, HIGH PERFORMANCE SUPERSONIC AIRCRAFT STRUCTURESWing and fuselage concepts for supersonic aircraft
Document ID
19630000199
Acquisition Source
Headquarters
Document Type
Other
Authors
Dunning, J. S. (Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Rowe, G. T. (Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Date Acquired
August 1, 2013
Publication Date
October 1, 1962
Subject Category
General
Report/Patent Number
DAC-31041
Report Number: DAC-31041
Accession Number
63N10072
Funding Number(s)
CONTRACT_GRANT: AF 33/657/-8541
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FATIGUE
ALLOY
WING
SUPERSONIC AIRCRAFT
FUSELAGE

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