NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
A study of the effect of adverse yawing moment on lateral maneuverability at a high lift coefficient
Document ID
19930092512
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Fehlner, Leo F
Date Acquired
September 6, 2013
Publication Date
September 1, 1942
Report/Patent Number
NACA-WR-L-465
Report Number: NACA-WR-L-465
Accession Number
93R21802
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CONTROL STICKS - FORCES
STABILITY, DIRECTIONAL
BANKING
WINGS - DIHEDRAL
MANEUVERABILITY
TAIL SURFACES, VERTICAL
LATERAL CONTROL DEVICES
SIDESLIPPING
AILERONS - DEFLECTION
LATERAL CONTROL & HIGH LIFT WORK CARRIED ON AT LAL
No Preview Available