A flight test determination of the static longitudinal stability of the Cessna 310d airplane
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Authors
Lenox, Glen W.
Lindell, Clifford A.
Subjects
Advisors
Perkins, Courtland D.
Date of Issue
1961-05
Date
May 1961
Publisher
Princeton University
Language
en_US
Abstract
The purpose of this investigation was to determine the static
longitudinal stability of the Cessna 310d airplane through steady state
flight tests.
The flight test method used to determine the location of the neutral
points was that in which the equilibrium elevator angle and stock
force were measured at various steady state airspeeds and center of
gravity locations. The maneuver points were determined from measurements
of equilibrium elevator angle and stick force for various load
factors and center of gravity locations in steady turns.
Type
Thesis
Description
This thesis document was issued under the authority of another institution, not NPS. At the time it was written, a copy was added to the NPS Library Collection for reasons not now known. It has been included in the digital archive for its historical value to NPS. Not believed to be a CIVINS (Civilian Institutions) title.
Series/Report No
Department
Aeronautical Engineering
Organization
Princeton University
Identifiers
NPS Report Number
Sponsors
Funder
Format
Citation
Distribution Statement
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.