Titlebook: Numerical Solutions of the Euler Equations for Steady Flow Problems; Albrecht Eberle,Arthur Rizzi,Ernst Heinrich Hirsch Book 1992 Springer

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Modelling of Vortex Flows: Vorticity in Euler Solutions,g. Ref. 2). With proper vortex sheet paneling, panel methods can also be employed on delta wings with leading-edge vortices, in this way allowing to compute non-linear lift problems with — linear — potential wing theory (see e.g. Ref. 3).

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Principles of Upwinding,ool for this purpose is the addition of a higher derivative of the flow variables, multiplied by a suited coefficient, to each line of the Euler equations. This is called the artificial viscosity approach, and is the topic of the preceding Chapter V.

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The Euler Equations,much smaller than the characteristic length of the object being immersed in the fluid flow, b) because the volume forces are usually much smaller than the global forces generated by the dynamics of the flow.

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Fundamentals of Discrete Solution Methods,tions and how they affect stability are also discussed.. The second part introduces basic ideas on discrete methods, their accuracy and consistency, numerical stability and numerical boundary conditions.

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Methods in Practical Applications,ese cases illustrate many different phenomena. Some are chosen to demonstrate the type and character of flow separation that is observed in Euler computations, other are chosen to demonstrate the practical utility of Euler solutions for industrial design.

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0179-9614 odynamics the classical potential-flow methods have been complemented by higher modelling-level methods. Euler solvers, and for special purposes, already Navier-Stokes solvers are in use. The authors of this book have been working on the solution of the Euler equations for quite some time. While the

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Numerical Solutions of the Euler Equations for Steady Flow Problems

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Albrecht Eberle,Arthur Rizzi,Ernst Heinrich Hirsch