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Damping in roll of models with 45, 60 and 70 degree delta wings determined at high subsonic, transonic, and supersonic speeds with rocket-powered models
Document ID
19930087208
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sanders, E Claude, Jr
Date Acquired
August 29, 2013
Publication Date
June 25, 1952
Report/Patent Number
NACA-RM-L52D22a
Report Number: NACA-RM-L52D22a
Accession Number
93R16498
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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