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 method for solution of aerodynamic forces on thin wings in nonuniform supersonic stream with an application to tail surfaces
Document ID
19930082432
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mirels, Harold
Date Acquired
August 16, 2013
Publication Date
November 1, 1948
Report/Patent Number
NACA-TN-1736
Report Number: NACA-TN-1736
Accession Number
93R11722
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THEORIES - WINGS
THEORIES -- FLOW LINEAR
TAIL SURFACES, HORIZONTAL - CHARACTERISTICS
WINGS, THIN - STABILITY
WINGS, THIN - CHARACTERISTICS
THEORIES -- FLOW SUPERSONIC
UPWASH
THEORIES - AIRFOILS THIN

Related Records

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