An Experimental Study of Several Wind Tunnel Wall Configurations Using Two V/STOL Model Configurations
Author | : T. W. Binion (Jr.) |
Publisher | : |
Total Pages | : 38 |
Release | : 1975 |
Genre | : Jet fighter planes |
ISBN | : |
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Author | : T. W. Binion (Jr.) |
Publisher | : |
Total Pages | : 38 |
Release | : 1975 |
Genre | : Jet fighter planes |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 882 |
Release | : 1975 |
Genre | : Government reports announcements & index |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 326 |
Release | : 1973 |
Genre | : Aeronautics |
ISBN | : |
Author | : B. F. R. Ewald |
Publisher | : |
Total Pages | : 578 |
Release | : 1998 |
Genre | : Aerodynamics |
ISBN | : |
This report was compiled by an international team of wind tunnel wall correction experts. It presents the present state of the art in wind tunnel wall corrections with a special emphasis given to the description of modern wall correction methods based on Computational Fluid Dynamics. This AGARDograph was planned by the AGARD Fluid Dynamics Panel to be a modern sequel of the successful AGARDograph 109 "Subsonic Wind Tunnel Wall Corrections", which was published in 1966. AGARDogaph 109 is still valid and continues to be used to provide wall corrections in many wind tunnels. Nevertheless, in the thirty two years since the publication of AGARDograph 109, much work has been done on the subject, and the influence of the new tool of numerical fluid dynamics was so strong, that a sequel to AGARDograph 109 was considered to be necessary.