EUROPT — A European Initiative on Optimum Design Methods in Aerodynamics: Proceedings of the Brite/Euram Project Workshop “Optimum Design in Areodynamics”, Barcelona, 1992: Notes on Numerical Fluid Mechanics, cartea 55
Editat de Jacques Periaux Contribuţii de Theo Labrujere Editat de Gabriel Bugeda, Panagiotis K. Chaviaropoulos, Bruno Stouffleten Limba Engleză Paperback – 14 feb 2012
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Specificații
ISBN-13: 9783322865724
ISBN-10: 332286572X
Pagini: 208
Ilustrații: VIII, 196 p.
Dimensiuni: 155 x 235 x 11 mm
Greutate: 0.3 kg
Ediția:Softcover reprint of the original 1st ed. 1997
Editura: Vieweg+Teubner Verlag
Colecția Vieweg+Teubner Verlag
Seria Notes on Numerical Fluid Mechanics
Locul publicării:Wiesbaden, Germany
ISBN-10: 332286572X
Pagini: 208
Ilustrații: VIII, 196 p.
Dimensiuni: 155 x 235 x 11 mm
Greutate: 0.3 kg
Ediția:Softcover reprint of the original 1st ed. 1997
Editura: Vieweg+Teubner Verlag
Colecția Vieweg+Teubner Verlag
Seria Notes on Numerical Fluid Mechanics
Locul publicării:Wiesbaden, Germany
Public țintă
ResearchCuprins
1. Introduction.- 2. Definition of the Problems for the Analysis.- 2.1 Test Case T1: Inverse Problem for a Nozzle.- 2.2 Test Case T2: Subsonic Optimization Problem for a Nozzle.- 2.3 Test Case T3: Transonic Optimization Problem for a Nozzle.- 2.4 Test Case T4: Inverse Problem for a 2D Single Airfoil.- 2.5 Test Case T6: Optimization Problem for a 2D Single Airfoil.- 2.6 Test Case T8: Test Case for Multi-Point 2D Airfoil Design.- 2.7 Test Case T10: Reconstruction Problem for a 2D Multi-Element Airfoil.- 2.8 Test Case T14: Design and Reconstruction Test Case for Single-Point 3D Wing Design.- 2.9 Test Case T17: Reconstruction Problem for a 3D Nozzle.- 3. Contributions to the Resolution of the Workshop Test Cases.- Contribution to problems T4 and T6 finite element GMRES and conjugate gradient solvers.- Wing design with a 3D-subsonic inverse panel method.- Direct optimization of transonic airfoils.- A residual correction method applied to 2D multi-point airfoil design and 3D single-point wing design.- Comparison of some optimization methods and their application in the shape optimization of lifting airfoils.- Shape optimization of an Euler flow in a nozzle.- Aerodynamic shape optimization using automatic adaptive remeshing.- Single-pass method for the solution of the 2D & 3D inverse potential problem.- 4. Description of the Graphic Software Used for the Workshop.- 5. Synthesis of the Workshop Test Cases.- 6. Conclusions and Further Comments.
Notă biografică
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Caracteristici
Internationales Forschungsprogramm