The effects of power on the stability and the control characteristics of an airplane are discussed and methods of analysis are given for evaluating certain dynamic characteristics of the airplane that are not directly discernible from wind tunnel tests alone. Data are presented to show how the characteristics of a model tested in a wind tunnel are affected by power. The response of an airplane to a rolling and a yawing disturbance is discussed, particularly in regard to changes in wing dihedral and fin area. Solutions of the lateral equations of motion are given in a form suitable for direct computations. An approximate formula is developed that permits the rapid estimation of the accelerations produced during pull-up maneuvers involving abrupt elevator deflections.
Methods of analyzing wind-tunnel data for dynamic flight conditions
1976-01-01
Sonstige
Keine Angabe
Englisch
WIND TUNNEL DATA ANALYZING BY JAVAD SOFTWARE
TIBKAT | 2020
|Calculation of tab characteristics for flight conditions from wind-tunnel data
Engineering Index Backfile | 1942
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