NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Effect of linear spanwise variations of twist and circular-arc camber on low-speed static stability, rolling, and yawing characteristics of a 45 degree sweptback wing of aspect ratio 4 and taper ratio 0.6
Document ID
19930083567
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Jaquet, Byron M
Date Acquired
August 16, 2013
Publication Date
August 1, 1952
Report/Patent Number
NACA-TN-2775
Report Number: NACA-TN-2775
Accession Number
93R12857
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