A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver /
Leonard Sternfield.

Description

Main Author

Sternfield, Leonard.

Related Names

Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1956.

Subjects

Charts, diagrams, etc.
Mathematics.
Airplanes > Airplanes / Control.
Rolling (Aerodynamics)
Calculations made with and without the derivatives for side force due to sideslip and lift-curve slope indicate that although these derivatives increase the total damping of the system they do not markedly affect the transient motion.

Summary

The transient motion in angles of attack and sideslip during a constant rolling maneuver has been analyzed. Simplified expressions are presented for the determination of the pertinent modes of motion as well as the modal coefficient corresponding to each mode.

Note

NACA Research Memorandum L56F04.
"August 28, 1956."
Title from cover.

Physical Description

38 p. : ill. ; 27 cm.

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