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Wind-tunnel Investigation of a Ram-jet Canard Missile Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Degree Swept Leading Edges : Longitudinal and Lateral Stability and Control Characteristics at a Mach Number of 1.60
Document ID
19930087863
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Spearman, M Leroy
Robinson, Ross B
Date Acquired
August 16, 2013
Publication Date
August 1, 1952
Report/Patent Number
NACA-RM-L52E15
Report Number: NACA-RM-L52E15
Accession Number
93R17153
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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