PREDICTION OF AERODYNAMIC COEFFICIENTS OF MISSILE USING PANEL METHOD
The low order panel method with Neumann boundary condition have been used to predict the normal force curve slope, the pitching moment curve slope, the center of pressure location and the aerodynamic load distribution for missile in compressible, steady flow. The wing-body-canard interference probl...
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| Autors principals: | , , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
University of Baghdad
2006-06-01
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| Col·lecció: | Journal of Engineering |
| Matèries: | |
| Accés en línia: | https://www.joe.uobaghdad.edu.iq/index.php/main/article/view/2870 |
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