In this report a study is made of the effect on longitudinal and lateral oscillations of an airplane of simultaneous variations in two resistance derivatives while the remainder of the derivatives are constant. The results are represented by diagrams in which the two variable resistance derivatives are used as coordinates, and curves are plotted along which the modulus of decay of a long oscillation has a constant value. The same type of analysis is also carried out for the stability of the parachute. In discussing the stability of the helicopter it is concluded that the gyroscopic effect on stability will be greater than in the case of the airplane.
Diagrams of airplane stability
01.01.1921
Sonstige
Keine Angabe
Englisch
Diagrams of airplane stability
Engineering Index Backfile | 1920
|Airplane as object of control (Block Diagrams of Equations of Perturbed Airplane Motion)
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