It does not calculate the derivatives for transonic and supersonic flow. The stability and control derivatives modules only deal with subsonic flow (up to about Mach0.7) for most derivatives. The detailed drag module allows designers to go all the way to supersonic flow. The AAA program allows students and preliminary design engineers to take an aircraft configuration from early weight sizing through open loop and closed loop dynamic stability and sensitivity analysis, while working within regulatory and cost constraints. This provides the designer with an instant appraisal of the status of the design relative to these regulations. All applicable performance and flying quality regulations are available in the AAA program.
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