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Wing Loads on the Bell X-1 Research Airplane (10 Percent Thick Wing) as Determined by Pressure-distribution Measurements in Flight at Subsonic and Transonic Speeds
Document ID
19930087661
Document Type
Other
Authors
Knapp, Ronald J
Jordan, Gareth H
Date Acquired
August 16, 2013
Publication Date
November 4, 1953
Report/Patent Number
NACA-RM-L53G14
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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