Calculation of the Lateral-Dynamic Stability of Aircraft
Description:
"Graphs and formulas are given with the aid of which all the aerodynamic coefficients required for computing the lateral dynamic stability can be determined. A number of numerical examples are given for obtaining the stability derivatives and solving the characteristic-stability equation. Approximate formulas are derived with the aid of which rapid preliminary computations may be made and the stability coefficients corrected for certain modifications of the airplane" (p. 1).
Date:
February 1952
Creator:
Raikh, A.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department