A method of determining the moments of inertia of an airplane from design data pertaining to the weights and locations of the component parts is described. The computations required to ascertain the center-of-gravity position are incorporated with the calculations of moments of inertia. A complete set of data and calculations for a modern airplane is given to illustrate the procedure. From a comparison between calculated values and measured values it is believed that the moments of inertia can be estimated within 10 percent by the use of this method.
Estimation of moments of inertia of airplanes from design data
01.07.1936
Sonstige
Keine Angabe
Englisch
Estimation of moments of inertia of airplanes from design data
Engineering Index Backfile | 1936
|Estimation of moments of inertia of airplanes from design data
TIBKAT | 1936
|Moments of inertia of airplanes
SLUB | 1931
|Moments of inertia of several airplanes
Engineering Index Backfile | 1931
|Moments of inertia of several airplanes
TIBKAT | 1931
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