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E-grāmata: Optimum Aerodynamic Design & Parallel Navier-Stokes Computations ECARP - European Computational Aerodynamics Research Project

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This volume entitled "European Computational Aerodynamics Research Project (ECARP)" contains the contributions of partners presented in two work­ shops focused on the following areas: Task 3 on Optimum Design and Task 4.2 on Navier Stokes Flow algorithms on Massively Parallel Processors. ECARP has been supported by the European Union (EU) through the Indus­ trial and Materials Technology Programme, Area 3 Aeronautics, with the Third Research Framework Programme (1990-1994). Part A of this volume is focused on computational constrained optimization as a follow up of the EU research project" Optimum Design in Aerodynamics" , (AERO-S9-0026) dealing with more viscous flow based real applications. It pro­ vides the reader with a set of optimization tools and referenced data useful in modern aerodynamic design. Task 3 of the project entitled "Optimum Design" brought together 13 Euro­ pean partners from the academic and industrial aeronautic oriented community showing state of the art expertise in traditional automated optimization software on current computer technology to improve the capability to optimize aircraft shapes.

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Springer Book Archives
A: Numerical Optimization in Aerodynamic Design.- I. Introduction.- II. Definition of the Problems for the Analysis.-
1. Definition of test cases.-
2. ECARP data base: access rules and storage formats.-
3. ECARP data base: visualization tools.- III. Contributions to the Resolution of the Data Workshop Test Cases.-
1. On the optimization of a wing-pylon-nacelle configuration.-
2. Optimization of transonic airfoils and wings.- 2.1 Optimization of transonic airfoils.- 2.2 Optimization of transonic wings.-
3. Airfoil optimization using viscous/inviscid coupling code.-
4. Optimization of the wing-pylon-nacelle testcase TE5 by HISSS-D, a panel method-based design tool.-
5. Design of a wing-pylon-nacelle configuration.-
6. Dassault contribution to the optimum design ECARP project.-
7. Geometry optimization of airfoils by multi-point design.-
8. Riblet optimization.-
9. Aerodynamic design of a M6 wing of transonic wing using unstructured meshes.-
10. Part I. Single and two-point airfoil design using Euler and Navier-Stokes equations.-
10. Part II. Application of genetic algorithms to the design of airfoil pressure distributions.-
11. Design and optimization aspects of 2-D and quasi 3-D configurations using an inverse Euler solver.-
12. Optimum aerodynamic shape design including mesh adaptivitiy.- IV. Synthesis of Test Cases.- V. Conclusion and Perspectives.- B: Navier Stokes Solution on MPP Computers.- I. Introduction.- II. Definition of the Problems for the Analysis.- III. Contribution to the Resolution of the Data Workshop Test Cases.-
1. Flow computation for a NACA0012 with the parallel Navier-Stokes Solver CGNS.-
2. Massively parallel computers for Navier-Stokes solutions on unstructured meshes.-
3. Parallel computations on an IBM SP2 and SGI cluster.- 3.1 Parallel computations on an IBM SP2 and an SGI cluster for the NACA0012 airfoil.- 3.2 Parallel computations on an IBM SP2 for the MW6 wing.-
4. Contributions from INRIA to the test cases.- 4.1 TP1 test case.- 4.2 TP2 test case.-
5. Viscous flow computations using structured and unstructured grids on the Intel-Paragon.-
6. Development of finite element algorithms for compressible viscous flows for parallel SIMD machines.-
7. Implementation of Navier-Stokes solvers on parallel computers.-
8. Navier Stokes simulations on MIMD computers using the EURANU Scode.- IV. Synthesis of Test Cases.- V. Conclusion and Perspectives.- Acknowledgements.- Annex: List of Partners and Addresses.
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