Calculation of the aileron and elevator stick forces and rudder pedal forces for the Bell XP-83 airplane (project MX-511) in spins /

Calculation of the aileron and elevator stick forces and rudder pedal forces for the Bell XP-83 airplane (project MX-511) in spins / by Ralph W. Stone. Jr., and Leslie E. Schneiter.

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Aileron and elevator stick forces and rudder pedal forces for the Bell XP-83 (project MX-511) airplane in spins have been calculated. The hinge-moment characteristics of the 0.14-scale models of the control surfaces of the XP-83 airplane in attitudes simulating spins, as determined in the Langley 4-...

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Bibliographic Details
Main Author: Stone, Ralph W., Jr
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Schneiter, Leslie E.
Other title:NACA Wartime Reports. Series L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1945]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L575.
Subjects:
Airplanes > Models > Testing.
Airplanes > Control surfaces.
Elevators (Airplanes)
Ailerons.
Spin (Aerodynamics)
Wind tunnel testing.
Charts, diagrams, etc.

Norlin Library - Basement - Government Information - US

Holdings details from Norlin Library - Basement - Government Information - US
Call Number: Y 3.N 21/5:11/L575
Y 3.N 21/5:11/L575 Available Place a Hold

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