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Effects of wing inboard plan-form modifications on lift, drag, and longitudinal stability at Mach numbers from 1.0 to 2.3 of a rocket-propelled free-flight model with a 52.5 degree sweptback wing of aspect ratio 3
Document ID
19930089916
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Henning, Allen B
Date Acquired
August 29, 2013
Publication Date
June 19, 1957
Report/Patent Number
NACA-RM-L57D29
Report Number: NACA-RM-L57D29
Accession Number
93R19206
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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