Interactive Computer-Aided Design Aircraft Flying Qualities Program. Volume II. Methods Formulation Manual.

摘要

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)