NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A low-speed experimental study of the directional characteristics of a sharp-nosed fuselage through a large angle-of-attack range at zero angle of sideslipStatic yawing moments and some instantaneous yawing moments are presented through a range of angle of attack at zero sideslip angle for a plain fuselage model having a sharp conical nose and for the fuselage with several nose modifications, one of which consisted of a ring located at different stations along the nose. Some circumferential pressure measurements at one station on the body at several angles of attack are also presented.
Document ID
19930083617
Document Type
Other
Authors
Letko, William
Date Acquired
August 16, 2013
Publication Date
March 1, 1953
Report/Patent Number
NACA-TN-2911
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PROTUBERANCES-BODIES
STABILITY, DIRECTIONAL-STATIC
BODIES

Available Downloads

NameType 19930083617.pdf STI