Computational Studies In Low Speed Rotor Aerodynamics

Recently, curved vortex elements have been developed for use in helicopter free wake calculations. As previously documented, these elements allow more efficient and accurate calculation of the wake-on-wake interactions than do traditional straight vortex elements. Curved elements have been applied here to the prediction of the rotor wake geometry and its associated inflow distribution in low speed forward flight. By coupling the wake model to a blade dynamic analysis, a simulation capable of predicting blade motion and hub moments in forward flight has been developed. The resulting code has been validated by successful predictions of the lateral flapping of articulated rotors in low speed level flight, and additional simulations of climb and descent have been undertaken. Successful correlation of other experimental data, including moments due to cyclic on hingeless rotors and -transient thrust response in hover, has given encouraging evidence of the capabilities of this code as a tool for analysis of the low speed regime.