Calculation of the lateral-dynamic stability of aircraft

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Summary: 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. A derivation of the lateral-dynamic-stability equations is included.
Collection: NASA Technical Reports Server (NTRS) Collection.
Note: Document ID: 19930093966.
Accession ID: 93R23292.
NACA-TM-1264.
Terms of Use and Reproduction: No Copyright.

View MARC record | catkey: 15428302

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