Experimental determination of the aerodynamic damping and stiffness in yaw stability derivatives of some motor vehicle shapes.

Author(s)
Russell, J.B.
Year
Abstract

Experiments have been to determine the damping and stiffness in yaw derivates using the free oscillation techniques on four models. Records of the damped oscillations in yaw angle have been analysed and used to deduce the derivatives. Tests were carried out for two pivot locations for each model. Results are presented and discussed.

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Publication

Library number
B 15645 fo / 91 /
Source

In: Kolloquium über Industrieaerodynamic, Aachen, 28- 30 Oktober 1974, p. 129-139, fig., graph., ref.

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