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
The Damping Due to Roll of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow
Document ID
19930082350
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Jones, Arthur L
Alksne, Alberta
Date Acquired
August 16, 2013
Publication Date
March 1, 1948
Report/Patent Number
NACA-TN-1548
Report Number: NACA-TN-1548
Accession Number
93R11640
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGS, DELTA
THEORIES - WINGS
DAMPING IN ROLL
LOAD DISTRIBUTION ,WING-SPAN
DOWNWASH
THEORIES - FLOW - SUPERSONIC
WINGS, RECTANGULAR
WINGS, SWEPTBACK
WINGS - STABILITY
THEORIES - FLOW - LINEAR

Related Records

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