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
Theoretical relations between the stability derivatives of a wing in direct and in reverse supersonic flow
Document ID
19930082616
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Harmon, Sidney M
Date Acquired
August 29, 2013
Publication Date
September 1, 1949
Report/Patent Number
NACA-TN-1943
Report Number: NACA-TN-1943
Accession Number
93R11906
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THEORIES - FLOW SUPERSONIC
THEORIES - FLOW LINEAR
WINGS, FLAT
THEORIES - WINGS SUPERSONIC
PITCHING MOMENTS - WINGS
WINGS - CHARACTERISTICS
WINGS - STABILITY
DAMPING IN PITCH
DAMPING IN ROLL
AIR FLOW - AIRFOILS REVERSED

Related Records

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