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
Investigation of Effects of Geometric Dihedral on Low-speed Static Stability and Yawing Characteristics of an Untapered 45 Degree Sweptback-wing Model of Aspect Ratio 2.61
Document ID
19930082294
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Queijo, M J
Jaquet, Byron M
Date Acquired
August 16, 2013
Publication Date
September 1, 1948
Report/Patent Number
NACA-TN-1668
Report Number: NACA-TN-1668
Accession Number
93R11584
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - NACA 0012
WINGS, SWEPTBACK - CHARACTERISTICS
WIND TUNNEL TESTS - NACA - STABILITY WORK CARRIED ON AT LAL
ROLLING, PITCHING & YAWING MOMENTS - WINGS, SWEPTBACK
AIRFOILS - ASPECT RATIO, SMALL
WINGS - DIHEDRAL
WINGS, SWEPTBACK - STABILITY
SIDESLIPPING

Related Records

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