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
Investigation of the Distribution of Lift, Drag, and Pitching Moment Between the Wing and Fuselage of a 1/30-scale Semispan Model of the Bell X-5 Airplane at a Mach Number of 1.24 by the Naca Wing-flow Method
Document ID
19930087995
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Morris, Garland J
Silsby, Norman S
Date Acquired
August 16, 2013
Publication Date
January 16, 1952
Report/Patent Number
NACA-RM-L51K27
Report Number: NACA-RM-L51K27
Accession Number
93R17285
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