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
An application of Falkner's surface-loading method to predictions of hinge-moment parameters for swept-back wings
Document ID
19930082190
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Jones, Arthur L
Sluder, Loma
Date Acquired
August 16, 2013
Publication Date
February 1, 1948
Report/Patent Number
NACA-TN-1506
Report Number: NACA-TN-1506
Accession Number
93R11480
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LOAD DISTRIBUTION - WINGS, SWEPTBACK
CONTROL SURFACES - HINGE MOMENTS
AIRFOILS - NACA 64A010 LOW-DRAG
THEORIES - AIRFOILS LIFTING-LINE
WINGS, SWEPTBACK
LIFT DISTRIBUTION, WING-SPAN - FALKNER METHOD
THEORIES - AIRFOILS LIFTING-SURFACE
LIFT DISTRIIBUTION - WINGS, SWEPTBACK
VORTICES, HORSESHOE

Related Records

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