NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Factors affecting the stability of T-tail transports.Wind tunnel research of deep stall aerodynamic characteristics of T tail analyzed as preliminary design guide
Document ID
19660057201
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Ray, E. J.
Taylor, R. T.
Date Acquired
August 3, 2013
Publication Date
August 1, 1966
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Aircraft
Report/Patent Number
AIAA PAPER 65-737
Report Number: AIAA PAPER 65-737
Accession Number
66A36491
Distribution Limits
Public
Copyright
Other
Keywords
WIND TUNNEL STABILITY TEST
T TAIL SURFACE
LONGITUDINAL STABILITY
AERODYNAMIC CHARACTERISTICS

Available Downloads

There are no available downloads for this record.
No Preview Available