Unsteady RAH-66 Comanche Flowfield Simulations Including Fan-in-Fin

Understanding the dynamic relationship between the antitorque moment thrust and the applied collective pitch angle is crucial especially for directional control sensitivity analyses. Although there are many studies in the literature on the steady state behavior of the FANTAIL TM , little is known about the transient response and thrust build up, which is the primary focus of this paper. Computational fluid dynamics is used for the solutions here, because it provides a more complete flowfield prediction, especially in low-power, near edge-wise conditions. The flowfield is assumed to be inviscid and the Euler equations are solved with a blade element model for the FANTAIL TM . The main rotor is excluded in this study. Solutions are obtained by modifying the computer code PUMA2 (Parallel Unstructured Maritime Aerodynamics), and using an unstructured grid of 2.8 million cells. It was run on the Beowulf clusters COCOA2 and COCOA3. Dynamic fan thrust and moment response to applied collective pitch in hover and forward flight are presented and discussed.