The Advanced Aircraft Analysis (AAA) software provides a powerful framework to support the iterative and nonunique process of aircraft preliminary design. The AAA program allows design engineers to rapidly evolve a preliminary aircraft configuration from early weight sizing through open-loop and closed-loop dynamic stability and sensitivity analysis, while working within civil and military regulations and cost constraints. AAA operates in either British or metric units.
The design methodology used in the development of the AAA program is based on Airplane Design, Parts I through VIII, and Airplane Flight Dynamics, Parts I and II, by Dr. Jan Roskam.
William Anemaat
Chief Engineer
Design, Analysis and Research Corporation
120 East 9th Street
Suite 2
Lawrence, KS 66044
USA
913-832-0434
913-832-0524 (fax)
For applications in related solution areas, see the following indices: Aerodynamics, Aerospace, Aircraft Design, Design Optimization, Engineering, the developer index for Design, Analysis and Research Corporation and the market segment index for Mechanical CAE.
