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Modeling of Natural Transition in Properly Three-Dimensional Flows

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Title: Modeling of Natural Transition in Properly Three-Dimensional Flows
Authors: Arthur, M
Horton, H
Mughal, MS
Item Type: Conference Paper
Abstract: The paper describes a method for viscous flow prediction which includes the prediction of transition onset location as an integral part of the calculation. The method is similar to others in that it is based on stability analysis of the boundary layers but acknowledges that solutions of the Reynolds-averaged Navier-Stokes (RANS) equations yield boundary layers of inadequate accuracy when conventional mesh sizes are used. The boundary layers are therefore recomputed to high accuracy by solving the laminar boundary layer equations. Transition onset locations determined by the stability analysis are passed back to the RANS solver for further iterations. The method described in this paper differs from others in that the laminar boundary layer calculation is fully three-dimensional and the stability analysis is through the fully three-dimensional parabolised stability equations for compressible flow. Results are presented to illustrate the capability of the laminar boundary layer method and the effectiveness of the method for solving the parabolised stability equations. In addition, preliminary validation results are presented from calculations of the viscous flow over the AFRL 1303 UCAV concept to demonstrate that the fully three-dimensional laminar boundary layer and stability analysis components can be combined successfully with a RANS method for calculating flows with natural transition.
Issue Date: 25-Jun-2009
Date of Acceptance: 22-Jun-2009
URI: http://hdl.handle.net/10044/1/30451
DOI: https://dx.doi.org/10.2514/6.2009-3556
Publisher: American Institute of Aeronautics and Astronautics
Journal / Book Title: AIAA 2009-3556
Copyright Statement: This conference paper was published prior to 1 July 2012, allowing the deposit of the final pdf. Copyright © 2009 by QinetiQ Ltd., Imperial College, London, and Horton Aerodynamics Ltd.. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.
Sponsor/Funder: QinetiQ Limited
Funder's Grant Number: CU004-27172
Conference Name: 39th AIAA Fluid Dynamics Conference
Publication Status: Published
Start Date: 2009-06-22
Finish Date: 2009-06-25
Conference Place: San Antonio, Texas
Appears in Collections:Applied Mathematics and Mathematical Physics
Faculty of Natural Sciences
Mathematics