Numerical Solution for Airfoils near Stall in Optimized Boundary-Fitted Curvilinear Coordinates-Reference-Cited by-同舟云学术

Numerical Solution for Airfoils near Stall in Optimized Boundary-Fitted Curvilinear Coordinates

Published:1979-05 Issue:5 Volume:17 Page:458-464
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Hodge James K.¹,Stone Alan L.²,Miller Thomas E.³

Affiliation:

1. Air Force Flight Test Center, Edwards Air Force Base, Calif.

2. Air Force Acquisitions Logistics Division, Wright-Patterson Air Force Base, Ohio

3. Air Force Flight Dynamics Laboratory, Wright-Patterson Air Force Base, Ohio

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.61155

Reference23 articles.

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

2. 2Thames, F. C. "Numerical Solution of the Incompressible Navier-Stokes Equations about Arbitrary Two-Dimensional Bodies," Ph.D. Thesis,Dept. of Aerophysics and Aerospace Engineering, Mississippi StateUniv.May 1975.

3. 3Hodge, J. K. "Numerical Solution of Incompressible Laminar Flow about Arbitrary Bodies in Body-Fitted Curvilinear Coordinates," Ph.D. Thesis,Dept. of Aerophysics and Aerospace Engineering, Mississippi StateUniv.Dec. 1975.

4. Solutions of the navier-stokes equations in various flow regimes on fields containing any number of arbitrary bodies using boundary-fitted coordinate systems

5. Stone, A. L. "A Numerical Solution of the Navier-Stokes Equations for Flow over an Arbitrary Airfoil," M.S. Thesis (GAE/AE/76D-5),Air Force Institute of Technology, Wright-Patterson AFB, Ohio,Dec. 1976.

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