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Results of Initial Wind-tunnel Flutter Experiments at Low Speed with a Towed Airplane Model Having a 40 Degree Sweptback Wing of Aspect Ratio 3.62 Equipped with Pylon-mounted Stores
Document ID
19930088508
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Martina, Albert P
Young, George E
Date Acquired
August 16, 2013
Publication Date
March 24, 1955
Report/Patent Number
NACA-RM-L54K17
Report Number: NACA-RM-L54K17
Accession Number
93R17798
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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