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Interactions of a propeller with a stator-induced circumferentially varying flow
Authors:John?Farnsworth  Email author" target="_blank">Michael?AmitayEmail author  David?Beal  Stephen?A?Huyer
Institution:(1) Mechanical Aerospace and Nuclear Engineering, Rensselaer Polytechnic Institute, 110 8th Street, Troy, NY, USA;(2) Center for Flow Physics and Control (CeFPaC), Rensselaer Polytechnic Institute, 110 8th Street, Troy, NY, USA;(3) Vehicle Dynamics and Signature Control, Code 8233, Naval Undersea Warfare Center, Division, Newport, RI 02841-1708, USA;(4) Present address: Department of Aeronautics, US Air Force Academy, Colorado Springs, CO 80840, USA;
Abstract:The interactions of a circumferentially varying stator cascade and a downstream fixed pitch propeller were investigated experimentally. The global performance of the components and the coupled system were systematically investigated through force and moment measurements on the propulsor model in a water tunnel. In addition, the wake of the cyclic stator cascade with and without the propeller was investigated downstream from a propulsor model using the Stereoscopic PIV technique. A cyclic distribution of the stators’ deflections resulted in non-axisymmetric distributions of the flow field downstream of the stator array. The stator distribution alone produced a significant side force that increased linearly with stator pitch amplitude. When a propeller was incorporated downstream from the cyclic cascade, the side force from the stator cascade was reduced, but a small normal force and pitching moment were created. The generation of these secondary forces and moments can be related to the redistribution of the tangential flow from the cyclic cascade into the axial direction by the retreating and advancing blade states of the fixed pitch propeller.
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