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Aeroacoustic Study of Coaxial Rotor under Varying Trim Conditions and Rotor Orientations using Free Wake Analysis
This paper performs aerodynamic and acoustic analysis on a coaxial rotor system based on the XH-59A coaxial helicopter. The aerodynamic analysis is performed in RCAS using free wake modeling, and the acoustic prediction is performed with PSU- WOPWOP, which utilizes Farassat's Formualation 1A of the
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