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Author | Title | Accn# | Year | Item Type | Claims |
| 1 |
Desideri, Jean-Antoine |
Hypersonic Flows for Reentry Problems |
I03342 |
1991 |
eBook |
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| 2 |
Periaux, Jacques |
Optimum Aerodynamic Design & Parallel Navier-Stokes Computations ECARP ??? European Computational Aerodynamics Research Project |
I03014 |
1998 |
eBook |
|
| 3 |
Periaux, Jacques |
EUROPT ??? A European Initiative on Optimum Design Methods in Aerodynamics |
I00803 |
1997 |
eBook |
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1.
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| Title | Hypersonic Flows for Reentry Problems : Volume II: Test Cases ??? Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22???25 January 1990 |
| Author(s) | Desideri, Jean-Antoine;Glowinski, Roland;Periaux, Jacques |
| Publication | Berlin, Heidelberg, Springer Berlin Heidelberg, 1991. |
| Description | XIII, 1230 p. 397 illus., 8 illus. in color : online resource |
| Abstract Note | This entry describes the experimental work conducted in the Department of Aeronautics at Imperial College in connection with Test Problems 1 and 2 of the "Workshop on Hypersonic Flows for Reentry Problems, Part I". These are defined as follows: Test Problem 1 Flow Over a Slender Cone Test Problem 2 Turbulent Base Flow The main requirement of this text is to present the experimental data for direct comparison with the predictions of CFD codes. We have therefore concentrated mainly on a factual statement of measuring techniques and results, together with an assessment of experimental accuracy. Future publications will be devoted to more extensive physical interpretations and discussions of the results. We have produced a large volume of data, some of which were categorised as "MANDATORY" and some as "OPTIONAL" for the purposes of CFD validation. However, only the "MANDATORY" data are presented here, although the other data are available and will be published separately later. 2. EXPERIMENTAL ARRANGEMENT 2. 1 The Test Facility The experiments were conducted in the Imperial College No. 2 Gun tunnel. This facility is a conventional intermittent blowdown tunnel with a contoured Mach 9 (nominal) axisymmetric nozzle fed by a free piston compression heater. The operating condition under which the data contained in this report were obtained is presented in Table 1. Test 2 T (oK) M b. Mlm Po (N/m ) Re/m T (oK) IX) IX) Case IX) w 1. 1 7 7 +0. 14 9. 16 6. 67x10 5. 5xl0 59 |
| ISBN,Price | 9783642765278 |
| Keyword(s) | 1. EBOOK
2. EBOOK - SPRINGER
3. Fluid- and Aerodynamics
4. FLUIDS
5. Mathematical Methods in Physics
6. NUMERICAL ANALYSIS
7. Numerical and Computational Physics, Simulation
8. PHYSICS
|
| Item Type | eBook |
Multi-Media Links
Please Click here for eBook
Circulation Data
| Accession# | |
Call# | Status | Issued To | Return Due On | Physical Location |
| I03342 |
|
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On Shelf |
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2.
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| Title | Optimum Aerodynamic Design & Parallel Navier-Stokes Computations ECARP ??? European Computational Aerodynamics Research Project |
| Author(s) | Periaux, Jacques;Bugeda, Gabriel;Giannakoglou, Kyriakos;Mantel, Bertrand |
| Publication | Wiesbaden, 1. Imprint: Vieweg+Teubner Verlag
2. Vieweg+Teubner Verlag, 1998. |
| Description | X, 467 p. 201 illus : online resource |
| Abstract Note | 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 |
| ISBN,Price | 9783322901934 |
| Keyword(s) | 1. APPLIED MATHEMATICS
2. Computational Mathematics and Numerical Analysis
3. Computer mathematics
4. EBOOK
5. EBOOK - SPRINGER
6. ENGINEERING MATHEMATICS
7. Fluid- and Aerodynamics
8. FLUIDS
9. Mathematical and Computational Engineering
|
| Item Type | eBook |
Multi-Media Links
Please Click here for eBook
Circulation Data
| Accession# | |
Call# | Status | Issued To | Return Due On | Physical Location |
| I03014 |
|
|
On Shelf |
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3.
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| Title | EUROPT ??? A European Initiative on Optimum Design Methods in Aerodynamics : Proceedings of the Brite/Euram Project Workshop ???Optimum Design in Areodynamics???, Barcelona, 1992 |
| Author(s) | Periaux, Jacques;Bugeda, Gabriel;Chaviaropoulos, Panagiotis K;Stoufflet, Bruno |
| Publication | Wiesbaden, 1. Imprint: Vieweg+Teubner Verlag
2. Vieweg+Teubner Verlag, 1997. |
| Description | VIII, 196 p : online resource |
| Abstract Note | This volume entitled "EUROPT - A European Initiative on Optimum Design in Aerodynamics" contains the results of the contributors during a workshop which took place in Barcelona in June 1992. This workshop was organized in the framp?? work of the Brite/Euram Aeronautics project "Optimum Design in Aerodynamics" (AERO-89-0026). The project brought together nine European partners from Acade?? my and Industry with big experience in numerical optimization techniques applif'd to automated optimum design. The manuscript is directed to the optimization field and its goal is to provide the reader with useful numerical optimization techniques for optimum design in aerody?? namIcs. The field of numerical optimization techniques has been growing since the early 50's. But only recently, with the recent advent of powerful computers. it has yielded real-life applications that demonstrate industrial potential for design purposes. Nowadays, optimization is at the stage where those scientists and engineers who have worked in the field are to be paid to apply numerical optimization to automated design of real problems, namely aerodynamic shapes in Aerospace Engineering. For the above reasons, it was evident that a Workshop on numerical optimization techniques for the validation of optimum design methods would be of interest to most of the partners involved in the AERO-S9-0026 project in order to compare in terms of accuracy and efficiency several optimization soft wares performed on the same selected flow problems |
| ISBN,Price | 9783322865700 |
| Keyword(s) | 1. APPLIED MATHEMATICS
2. Computational Mathematics and Numerical Analysis
3. Computer mathematics
4. EBOOK
5. EBOOK - SPRINGER
6. ENGINEERING MATHEMATICS
7. Fluid- and Aerodynamics
8. FLUIDS
9. Mathematical and Computational Engineering
|
| Item Type | eBook |
Multi-Media Links
Please Click here for eBook
Circulation Data
| Accession# | |
Call# | Status | Issued To | Return Due On | Physical Location |
| I00803 |
|
|
On Shelf |
|
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