Inverse mode calculations of the incompressible turbulent boundary layer on an ellipsoid
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9493
Reference18 articles.
1. Boundary-Layer Calculations in the Inverse Mode for Incompressible Flows over Infinite Swept Wings
2. A method for designing three-dimensional configurations with prescribed skin friction
3. The application of inverse boundary layer methods to the three-dimensional viscous design problem
4. Singularities in three-dimensional turbulent boundary-layer calculations and separation phenomena
5. A finite difference method for inverse solutions of 3-D turbulent boundary-layer flow
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1. Experimental study of three-dimensional separation on a large-scale model;AIAA Journal;1995-11
2. Experimental study of 3-D separation on a large scale model;23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference;1993-07-06
3. Navier-Stokes computations past a prolate spheroid at incidence—I. Low incidence case;Computers & Fluids;1992-10
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5. On three-dimensional flow separation criteria;22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference;1991-06-24
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