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
Effects of Reynolds number and leading-edge shape on the low-speed longitudinal stability of a 6-percent-thick 45 degree sweptback wing
Document ID
19930089158
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schneider, William C
Date Acquired
August 16, 2013
Publication Date
April 18, 1956
Report/Patent Number
NACA-RM-L56B14
Report Number: NACA-RM-L56B14
Accession Number
93R18448
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