The numerical solution of incompressible turbulent flow over airfoils-Reference-Cited by-同舟云学术

The numerical solution of incompressible turbulent flow over airfoils

Published:1981-01-12 Issue: Volume: Page:
ISSN:
Container-title:19th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

HEGNA H.¹

Affiliation:

1. USAF, Wright Aeronautical Laboratories, Wright-Patterson AFB, Ohio

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1981-47

Reference49 articles.

1. Automatic numerical generation of body-fitted curvilinear coordinate system for field containing any number of arbitrary two-dimensional bodies

2. Walker, R. L. "Nmerical Solution of the Navier-Stokes Equations for Incompressible Viscous Laminar Flow Past a Semi-Infinite Flat Plate", MS Thesis,Mississippi State Univ., 1974.

3. Thames, F. C. University, 1975.

4. Starting vortex, separation bubbles and stall: a numerical study of laminar unsteady flow around an airfoil

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2. Rough-wall layer modeling using the Brinkman equation;Journal of Turbulence;2009-01

3. Reply by Authors to M.S. Raju, M.J. Creed, and L. Krishnamurthy;AIAA Journal;1986-04

4. Numerical prediction of dynamic forces on arbitrarily pitched airfoils in turbulent flow;20th Aerospace Sciences Meeting;1982-01-11

5. Numerical Solution of Incompressible Turbulent Flow over Airfoils near Stall;AIAA Journal;1982-01