NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Effect of Taper Ratio on Low-speed Static and Yawing Stability Derivatives of 45 Degree Sweptback Wings with Aspect Ratio of 2.61
Document ID
19930082298
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Letko, William
Cowan, John W
Date Acquired
August 16, 2013
Publication Date
July 1, 1948
Report/Patent Number
NACA-TN-1671
Report Number: NACA-TN-1671
Accession Number
93R11588
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL TESTS - NACA - STABILITY WORK CARRIED ON AT LAL
ROLLING, PITCHING & YAWING MOMENTS - WINGS, SWEPTBACK
WINGS, SWEPTBACK - STABILITY
AIRFOIILS - NACA 0012
WINGS, SWEPTBACK - TAPERED
WINGS, SWEPTBACK - CHARACTERISTICS

Related Records

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