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Experimental and computational study of the flow induced by a plasma actuator
Institution:1. Department of Mechanical Engineering, Technische Universität Darmstadt, Germany;2. Institute of Fluid Mechanics and Aerodynamics (SLA), Petersenstrasse 17, D-64287 Darmstadt, Germany;3. Center of Smart Interfaces (CSI), Petersenstrasse 17, D-64287 Darmstadt, Germany;1. Air Force Engineering University, 710038 Xi’an, PR China;2. Xi’an Jiaotong University, 710049 Xi’an, PR China;3. Tsinghua University, 100084 Beijing, PR China;1. State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang, China;2. Low Speed Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang, China;1. Institut PPRIME, Université de Poitiers, Bd Marie et Pierre Curie, BP 30179, Teléport 2, Chasseneuil Cedex, France;2. Departamento de Física Aplicada III, Universidad de Sevilla, ESI, Camino de Los Descubrimientos s/n, 41092 Sevilla, Spain
Abstract:A complementary experimental and computational study of the flow field evoked by a plasma actuator mounted on a flat plate was in focus of the present work. The main objective of the experimental investigation was the determination of the vector force imparted by the plasma actuator to the fluid flow. The force distribution was presently extracted from the Navier–Stokes equations directly by feeding them with the velocity field measured by a PIV technique. Assuming a steady-in-mean, two-dimensional flow with zero-pressure gradient, the imbalance between the convective term and the momentum equation’s right-hand-side terms reveals the desired resulting force. This force-distribution database was used afterwards as the source term in the momentum equation. Furthermore, an empirical model formulation for the volume-force determination parameterized by the underlying PIV-based model is derived. The model is tested within the RANS framework in order to predict a wall jet-like flow induced by a plasma actuator. The Reynolds equations are closed by a near-wall second-moment closure model based on the homogeneous dissipation rate of the kinetic energy of turbulence. The computationally obtained velocity field is analysed along with the experimental data focussing on the wall jet flow region in proximity of the plasma actuator. For comparison purposes, different existing phenomenological models were applied to evaluate the new model’s accuracy. The comparative analysis of all applied models demonstrates the strength of the new empirical model, particularly within the plasma domain. In addition, the presently formulated empirical model was applied to the flow in a three-dimensional diffuser whose inflow was modulated by a pair of streamwise vortices generated by the present plasma actuator. The direct comparison with existing experimental data of Grundmann et al. (2011) demonstrated that the specific decrease of the diffuser pressure corresponding to the continuous forcing was predicted correctly.
Keywords:Plasma actuator  Wall jet  PIV-based volume-force model  Second-moment closure RANS model  Three-dimensional diffuser
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