Interactive Computer-Aided Design Aircraft Flying Qualities Program. Volume II. Methods Formulation Manual.
Final rept., 1 Jan-Aug 74,
GENERAL DYNAMICS/CONVAIR SAN DIEGO CALIF
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This report describes a digital computer program which calculates the longitudinal and lateral-directional stability and control derivatives and aircraft flying qualities for a Mach number range for 0 - 3.0. The report consists of four volumes. Volume II, Methods Formulation Manual, outlines the methodology and source, range of applicability, and modifications. Modified author abstract