NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Effect of Horizontal-tail Position on the Hinge Moments of an Unbalanced Rudder in Attitudes Simulating Spin Conditions
Document ID
19930081964
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Note
Authors
Stone, Ralph W , Jr
Burk, Sanger M , Jr
Date Acquired
August 16, 2013
Publication Date
June 1, 1947
Report/Patent Number
NACA-TN-1337
Report Number: NACA-TN-1337
Accession Number
93R11254
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
RUDDER CONTROLS - FORCES
RUDDERS - HINGE MOMENTS
TAIL SURFACES - POSITION
TAIL SURFACES, VERTICAL - HINGE MOMENTS
TAIL SURFACES, HORIZONTAL - HINGE MOMENTS
WIND TUNNEL TESTS - NACA - FREE-SPINNING (15')
AIRFOILS - NACA 0009 - TAIL SURFACE
SPINNING - RECOVERY
SPINNING CHARACTERISTICS - EFFECT OF TAIL SURFACE
No Preview Available