Description: We propose the development of a modern panel code for calculation of steady and unsteady aerodynamic loads needed for dynamic servoelastic (DSE) analysis of flight vehicles. The code will be especially tailored to be robust, reliable, and integrated with the NASA Object Oriented Optimization (O3) system through selection of analysis methods, file formats, and computing environment, allowing it to be efficiently applied to numerous problems of interest to NASA and industry.

Benefits: Potential NASA applications will include the use of the developed technology for design of any new generation aircraft or RLV system including complex and novel configurations such as blended wing-bodies, truss-braced wing configurations, low-boom supersonic configurations, etc.

This technology is expected to have commercial applications to aircraft design of subsonic transports, supersonic vehicles, bombers, fighters, UAV's, and general aviation airplanes. As such, it is expected to have significant commercial applications in airplane structural design, primarily with DoD, NASA, and the prime contractors.