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Effect of Leading-edge Droop on the Aerodynamic and Loading Characteristics of a 4-percent-thick Unswept-wing--fuselage Combination at Transonic Speeds
Document ID
19930089119
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schmeer, James W
Date Acquired
August 16, 2013
Publication Date
May 23, 1956
Report/Patent Number
NACA-RM-L56C14
Report Number: NACA-RM-L56C14
Accession Number
93R18409
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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