Numerical solution of differential equations of airplane motion in potential flow field (Q2724056)
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scientific article; zbMATH DE number 1615372
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Numerical solution of differential equations of airplane motion in potential flow field |
scientific article; zbMATH DE number 1615372 |
Statements
8 July 2001
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panel method
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Numerical solution of differential equations of airplane motion in potential flow field (English)
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The author investigates the airplane motion in a subsonic and supersonic potential flow. Aerodynamical forces and moments are calculated based on potential flow theory by the panel method. Boundary conditions on the airplane surface are modified by introducing the influence of angular velocity. The resulting system of equations is solved using the Runge-Kutta method.
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