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Effects of chord-extension and droop of combined leading edge flap and chord-extension on low-speed static longitudinal stability characteristics of an airplane model having a 35 degree sweptback wing with plain flaps neutral or deflected
Document ID
19930087398
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Jaquet, Byron M
Date Acquired
August 29, 2013
Publication Date
January 28, 1953
Report/Patent Number
NACA-RM-L52K21a
Report Number: NACA-RM-L52K21a
Accession Number
93R16688
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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