NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Effect of High-lift Devices on the Low-speed Static Lateral and Yawing Stability Characteristics of an Untapered 45 Degrees Sweptback Wing
Document ID
19930085454
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lichtenstein, Jacob H
Date Acquired
August 16, 2013
Publication Date
September 30, 1948
Report/Patent Number
NACA-RM-L8G20
Report Number: NACA-RM-L8G20
Accession Number
93R14744
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available