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Wind-tunnel Investigation of a Ram-jet Missile Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Degrees Swept Leading Edges : Force and Moment Characteristics at Combined Angles of Pitch and Sideslip for Mach Number 2.01
Document ID
19930089240
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Driver, Cornelius
Hamilton, Clyde V
Date Acquired
August 16, 2013
Publication Date
April 26, 1956
Report/Patent Number
NACA-RM-L56B21
Report Number: NACA-RM-L56B21
Accession Number
93R18530
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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