Numerical Methods for the Computation of Inviscid Transonic Flows with Shock Waves: A GAMM Workshop: Notes on Numerical Fluid Mechanics, cartea 3
Autor Arthur Rizzi, Henri Viviandde Limba Germană Paperback – 1981
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Specificații
ISBN-13: 9783528080778
ISBN-10: 3528080779
Pagini: 284
Ilustrații: XVI, 266 S. 30 Abb.
Dimensiuni: 155 x 235 x 15 mm
Greutate: 0.4 kg
Ediția:Softcover reprint of the original 1st ed. 1981
Editura: Vieweg+Teubner Verlag
Colecția Vieweg+Teubner Verlag
Seria Notes on Numerical Fluid Mechanics
Locul publicării:Wiesbaden, Germany
ISBN-10: 3528080779
Pagini: 284
Ilustrații: XVI, 266 S. 30 Abb.
Dimensiuni: 155 x 235 x 15 mm
Greutate: 0.4 kg
Ediția:Softcover reprint of the original 1st ed. 1981
Editura: Vieweg+Teubner Verlag
Colecția Vieweg+Teubner Verlag
Seria Notes on Numerical Fluid Mechanics
Locul publicării:Wiesbaden, Germany
Public țintă
ResearchCuprins
Boundary Conditions for Problems in Aerodynamics.- Accelerated Finite-Volume Calculation of Transonic Potential Flows.- Solution of the Transonic Full Potential Equation in Conservative Form Using an Implicit Algorithm.- Relaxation Method for the Full-Potential Equation.- Computation of Steady Inviscid Transonic Flows Using Pseudo-Unsteady Methods.- Transonic Flow Computation by a Multi-Grid Method.- Transonic Flow Computations with Finite Elements.- Transonic Flow Computations by a Variational Principle Finite Element Method.- A Finite Element Method for Computing Transonic Potential Flow.- Flow Calculations Using the Non-Conservative Potential Equation.- Test Problems for Inviscid Transonic Flow.- A Modification to the Method of Garabedian and Korn.- A Physically Consistent Time-Dependent Method for the Solution of the Euler Equations in Transonic Flow.- Numerical Solutions of the Euler Equations for Steady Transonic Flow Past a Lifting Aerofoil.- Finite-Volume Methods for the Solution of Euler Equations.- Computation of Rotational Transonic Flow.- Collective Comparison of the Solutions to the Workshop Problems.- A. Computational Mesh for Transonic Airfoils: The Standard Mesh.- B. Other Mesh Systems Used by the Participants.- C. Nonuniqueness of FCPOT Numerical Solution.