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Experimental and predicted longitudinal response characteristics of a large flexible 35-degree swept-wing airplane at an altitude of 35,000 feet
Document ID
19930088505
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Cole, Henry A
Brown, Stuart C
Holleman, Euclid C
Date Acquired
August 29, 2013
Publication Date
November 26, 1954
Report/Patent Number
NACA-RM-A54H09
Report Number: NACA-RM-A54H09
Accession Number
93R17795
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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