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We present results from our work to explore the viability of using parallel computers to solve multidisciplinary problems relevant to the definition of low noise, high-performance, low vibration rotorcraft. Our work has addressed issues related to the performance and scalability of parallel computers with respect to the rotor design process. We describe our recent work to couple parallel versions of a comprehensive rotor analysis code, a rotor aerodynamics code and a rotor optimization code to implement a two-level parallel rotor optimization strategy.

A two-level parallel strategy for rotorcraft optimization and design