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
Wind tunnel investigation of effect of yaw on lateral-stability characteristics IV : symmetrically tapered wing with a circular fuselage having a wedge-shaped rear and a vertical tail
Document ID
19930092566
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Wallace, Arthur R
Date Acquired
September 6, 2013
Publication Date
March 1, 1942
Report/Patent Number
NACA-WR-L-520
Report Number: NACA-WR-L-520
Accession Number
93R21856
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MONOPLANES, MID-WING VS HIGH- & LOW-WING
WINGS, TAPERED - CHARACTERISTICS EFFECT OF WING FLAPS
ROLLING & YAWING MOMENTS - AIRFOILS - NACA 23012
INTERFERENCES - WINGS & FUSELAGES
WING FLAPS, SPLIT - PARTIAL-SPAN (20% CHORD)
WINGS - STABILITY, LATERAL
FUSELAGES, CIRCULAR-WEDGE-SHAPED REAR
TAIL SURFACES, VERTICAL
STABILITY, DIRECTIONAL

Related Records

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