Evaluation of the longitudinal static stability of the US-2A aircraft.
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Authors
Cooper, Paul William
Subjects
Advisors
Layton, Donald
Date of Issue
1970-04
Date
Publisher
Naval Postgraduate School
Language
en_US
Abstract
An evaluation of the longitudinal static stability of a Navy-
US- 2A aircraft was made. The aircraft was equipped with a Data
Acquisition System capable of sensing and recording aerodynamic
data other than that given by the standard cockpit instruments.
Recorded data were displayed graphically and the Neutral Points
for stick-free stability and stick-fixed stability we re determined.
Stick-free static margin and stick-fixed static margin were
determined and evaluated.
Type
Thesis
Description
Series/Report No
Department
Aeronautics
Organization
Naval Postgraduate School