NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Longitudinal Stability and Control Characteristics at Mach Numbers of 1.41 and 2.01 of a 67 Degree Swept-wing Airplane Configuration with Canard Control Surfaces
Document ID
19930090148
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Spearman, M Leroy
Robinson, Ross B
Date Acquired
August 16, 2013
Publication Date
July 7, 1958
Report/Patent Number
NACA-RM-L58E20
Report Number: NACA-RM-L58E20
Accession Number
93R19438
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available