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Author | Title | Accn# | Year | Item Type | Claims |
| 1 |
Smits, Alexander J |
Turbulent Shear Layers in Supersonic Flow |
I06711 |
2006 |
eBook |
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| 2 |
Dervieux, Alain |
Computation and Comparison of Efficient Turbulence Models for Aeronautics ??? European Research Project ETMA |
I00844 |
1998 |
eBook |
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1.
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| Title | Turbulent Shear Layers in Supersonic Flow |
| Author(s) | Smits, Alexander J;Dussauge, Jean-Paul |
| Publication | New York, NY, Springer New York, 2006. |
| Description | XIV, 410 p. 171 illus : online resource |
| Abstract Note | A good understanding of turbulent compressible flows is essential to the design and operation of high-speed vehicles. Such flows occur, for example, in the external flow over the surfaces of supersonic aircraft, and in the internal flow through the engines. Our ability to predict the aerodynamic lift, drag, propulsion and maneuverability of high-speed vehicles is crucially dependent on our knowledge of turbulent shear layers, and our understanding of their behavior in the presence of shock waves and regions of changing pressure. Turbulent Shear Layers in Supersonic Flow provides a comprehensive introduction to the field, and helps provide a basis for future work in this area. Wherever possible we use the available experimental work, and the results from numerical simulations to illustrate and develop a physical understanding of turbulent compressible flows |
| ISBN,Price | 9780387263052 |
| Keyword(s) | 1. EBOOK
2. EBOOK - SPRINGER
3. Engineering Fluid Dynamics
4. FLUID MECHANICS
5. Fluid- and Aerodynamics
6. FLUIDS
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 |
| I06711 |
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On Shelf |
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2.
|  |
| Title | Computation and Comparison of Efficient Turbulence Models for Aeronautics ??? European Research Project ETMA |
| Author(s) | Dervieux, Alain;Braza, Marianna;Dussauge, Jean-Paul |
| Publication | Wiesbaden, 1. Imprint: Vieweg+Teubner Verlag
2. Vieweg+Teubner Verlag, 1998. |
| Description | XIV, 581 p. 385 illus : online resource |
| Abstract Note | The computation of complex turbulent flows by statistical modelling has already a long history. The most popular two-equation models today were introduced in the early sev?? enties. However these models have been generally tested in rather academic cases. The develope?? ment of computers has led to more and more acurate numerical methods. The interactions betwe~n numerical and modelling techniques are generally not well mastered. Moreover, computation of real life cases, including 3D effects, complex geometries and pressure gra?? dients based on two-equation models with low-Reynolds treatment at the proximity of walls are not really of common use. A large number of models has been proposed; this is perhaps the sign that none of them is really satisfactory, and then the assessment of their generality is not an easy task: it requires a lot of understanding of the physics and a lot of work for testing the large number of relevant cases in order to assess their limits of validity which is a condition for an improved confidence in engineering applications. This is probably why workshops and working groups are frequent and the ETMA consor?? tium has choosen to build a state of the art in theoretical and numerical statistical turbu?? lence modelling for real life computations by taking some marks with respect to previous workshops such as the Stanford meetings (1980,1981); some problems are kept or updated by new experiments, some problems are discarded, some new problems are introduced; the focus is kept on flows with 2D geometries |
| ISBN,Price | 9783322898593 |
| Keyword(s) | 1. Aerospace engineering
2. Aerospace Technology and Astronautics
3. ASTRONAUTICS
4. Computational Mathematics and Numerical Analysis
5. Computer mathematics
6. EBOOK
7. EBOOK - SPRINGER
8. Fluid- and Aerodynamics
9. FLUIDS
|
| Item Type | eBook |
Multi-Media Links
Please Click here for eBook
Circulation Data
| Accession# | |
Call# | Status | Issued To | Return Due On | Physical Location |
| I00844 |
|
|
On Shelf |
|
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