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Aeromechanics of Rigid Coaxial Rotor Models for Wind-Tunnel Testing
Journal of Aircraft, 2017A comprehensive analysis for evaluating performance and vibratory loads of a coaxial helicopter rotor is developed and validated against existing experimental data.
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A computational fluid dynamics (CFD) solver based on Reynolds-averaged Navier–Stokes (RANS) equations and high-efficiency trim model is used to simulate the unsteady aerodynamics of coaxial rotor. Farassat 1 A equations are adopted for predicting rotor far-field aerodynamic noise.
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High-efficiency hybrid trim method for CFD simulation of rigid coaxial rotor
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