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Spin-tunnel Investigation of a Model of a 60 Degree Delta-wing Airplane to Determine the Spin, Recovery, and Longitudinal Trim Characteristics Throughout an Extensive Range of Mass Loadings
Document ID
19930086108
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Klinar, Walter J
Jones, Ira P , Jr
Date Acquired
August 16, 2013
Publication Date
February 15, 1950
Report/Patent Number
NACA-RM-L9L06
Report Number: NACA-RM-L9L06
Accession Number
93R15398
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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