Stability and Control Methodology for Conceptual Aircraft Design. Volume 1. Methodology Manual.
Final rept. Jun 85-Jun 87,
AIR FORCE WRIGHT AERONAUTICAL LABS WRIGHT-PATTERSON AFB OH
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This report contains methodology for predicting stability and control characteristics of conceptual flight vehicles. The methodology presented is a combination of existing methodology, modified existing methodology, and newly developed methodology. The methodology is divided into three main sections 1 Aerodynamics of Longitudinal stability coefficients, 2 Lateral Stability coefficients, and 3 Static and Dynamic Stability Analysis. Keywords Aerodynamics, Trim drag.