Abstract
A grid fin is an unconventional aerodynamic lifting and control device consisting of an outer frame with internal grid framework of small chord. Present study performs the Navier-Stokes computations for the steady subsonic and supersonic turbulent flow past (a) grid fin alone (b) fin/body combination shapes. Efficient Grid-generation procedures are proposed for fin alone and for fin/body combination configurations. Full Navier-Stokes Equations with pointwise version of Baldwin-Barth one equation turbulence model are solved by an algorithm in a fully coupled, implicit, and large block structure. The computed results are in good agreement with the experimental data and detailed shock-shock interaction structure near grid fins can be obtained and examined. © 2002 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
| Original language | English |
|---|---|
| Title of host publication | 20th AIAA Applied Aerodynamics Conference |
| Publication status | Published - 2002 |
| Externally published | Yes |
| Event | 20th AIAA Applied Aerodynamics Conference 2002 - St. Louis, MO, United States Duration: 24 Jun 2002 → 26 Jun 2002 |
Conference
| Conference | 20th AIAA Applied Aerodynamics Conference 2002 |
|---|---|
| Place | United States |
| City | St. Louis, MO |
| Period | 24/06/02 → 26/06/02 |
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