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ART - Advanced Rotocraft Technology SIN 871-3 System Design, Engineering and Integration

ART - Advanced Rotocraft Technology SIN 871-4 Test and Evaluation

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SIN 871-4 Project 4: Enhanced Rotorcraft Aerodynamic Modules to Support Flight Testing

Summary of Services Performed: Develop computationally scalable software to utilize massively parallel computer systems to efficiently predict performance and stability in support of flight testing.

This project was to provide computationally scalable tools to predict rotorcraft performance, stability, and control. The ability to efficiently predict vehicle performance, stability, and control from high fidelity computer models would greatly enhance the design and testing process and improved the quality of system acquisition. Through this development, the US Navy Test Pilot School performance, stability, and control test procedures were fully implemented in a high performance parallel computing environment.

 

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