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Distribution of lift and pitching moment between wing and fuselage and effects of wing flexibility and dive brake on a 1/30-scale semispan model of the Bell X-5 airplane at transonic speeds as determined by the NACA wing-flow method
Document ID
19930088113
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Morris, Garland J
Silsby, Norman S
Date Acquired
August 29, 2013
Publication Date
March 23, 1954
Report/Patent Number
NACA-RM-L54A11
Report Number: NACA-RM-L54A11
Accession Number
93R17403
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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