Effect of elevator-profile modifications and trailing-edge strips on elevator hinge-moment and other aerodynamic characteristics of a full-scale horizontal tail surface /

Effect of elevator-profile modifications and trailing-edge strips on elevator hinge-moment and other aerodynamic characteristics of a full-scale horizontal tail surface / by Carl F. Schueller, Peter F. Korycinski, and H. Kurt Strass.

Show other versions (792)

Results are presented of tests of a full-scale horizontal tail surface made to determine the effect of elevator-profile modifications and trailing-edge strips on the elevator hinge-moment characteristics for elevators having fixed plan form and constant balance.

Saved in:
Bibliographic Details
Main Author: Schueller, Carl F.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Korycinski, Peter F., Strass, H. Kurt
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. L111.
Subjects:
Airplanes > Control surfaces.
Fighter planes.
Airplanes > Tail surfaces.
Elevators (Airplanes)
Hinge moments (Aerodynamics)
Trailing edges (Aerodynamics)
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/L111
Y 3.N 21/5:11/L111 Available Place a Hold

Similar Items