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Shock wave-boundary-layer interactions /
"This is the first book devoted solely to the phenomenon of Shock Wave Boundary Layer Interactions and covers all flow regimes where SBLI's occur"--Provided by publisher
| Clasificación: | Libro Electrónico |
|---|---|
| Otros Autores: | , |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Cambridge ; New York :
Cambridge University Press,
2011.
|
| Colección: | Cambridge aerospace series.
|
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 245 | 0 | 0 | |a Shock wave-boundary-layer interactions / |c edited by Holger Babinsky, John K. Harvey. |
| 260 | |a Cambridge ; |a New York : |b Cambridge University Press, |c 2011. | ||
| 300 | |a 1 online resource (xvii, 461 pages) : |b illustrations | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a computer |b c |2 rdamedia | ||
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| 490 | 1 | |a Cambridge aerospace series | |
| 520 | |a "This is the first book devoted solely to the phenomenon of Shock Wave Boundary Layer Interactions and covers all flow regimes where SBLI's occur"--Provided by publisher | ||
| 520 | |a "Shock Wave/Boundary Layer Interaction (SBLI) is a fundamental phenomenon in gas dynamics and frequently a defining feature in high speed aerodynamic flowfields. The interactions can be found in practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLI's have the potential to pose serious problems and is thus a critical issue for aerospace applications. This is the first book devoted solely to a comprehensive, state of the art explanation of the phenomenon with coverage of all flow regimes where SBLI's occur. The book includes contributions from leading international experts who share their insight into SBLI physics and the impact of these interactions on practical flow situations. This book is aimed at practitioners and graduate students in aerodynamics who wish to familiarise themselves with all aspects of SBLI flows. It is a valuable resource for the specialist because it gathers experimental, computational and theoretical knowledge in one place"--Provided by publisher | ||
| 504 | |a Includes bibliographical references and index. | ||
| 588 | 0 | |a Print version record. | |
| 505 | 0 | 0 | |t Introduction / |r John K. Harvey and Holger Babinsky -- |t Physical introduction / |r Jean Delery -- |t Transonic shock wave boundary layer interactions / |r Holger Babinsky and Jean Delery -- |t Ideal gas shock wave turbulent boundary layer interactions in supersonic flows and their modeling -- two dimensional interactions / |r Alexander A. Zheltovodov and Doyle D. Knight -- |t Ideal gas shock wave turbulent boundary layer interactions in supersonic flows and their modeling -- three dimensional interactions / |r Doyle D. Knight and Alexander A. Zheltovodov -- |t Experimental studies of shock wave/boundary layer interactions in hypersonic flows / |r Michael S. Holden -- |t Numerical simulation of hypersonic shock wave boundary layer interactions / |r Graham V. Candler -- |t Shock wave/boundary layer interactions taking place in hypersonic flows / |r John K. Harvey -- |t Shock wave unsteadiness in turbulent shock wave boundary layer interactions / |r P. Dupont, J.F. Debieve and J.P. Dussauge -- |t Analytical treatment of shock/boundary layer interactions / |r George Inger. |
| 505 | 0 | |a Cover; Title; Copyright; Dedication; Contents; Contributors; 1 Introduction; 1.1 Structure of the Book; 1.1.1 George Inger; 1.2 Intended Audience; 2 Physical Introduction; 2.1 Shock Wave-Boundary-Layer Interactions: Why They Are Important; 2.2 Discontinuities in Supersonic Flows; 2.2.1 Shock Waves; 2.2.2 The Shock-Polar Representation; 2.2.3 Shock Intersections and the Edney Classification of Shock-Shock Interferences; 2.2.4 Shock Waves, Drag, and Efficiency: The Oswatitsch Relationship; 2.3 On the Structure of a Boundary-Layer Flow; 2.3.1 Velocity Distribution through a Boundary Layer. | |
| 505 | 8 | |a 2.3.2 The Multilayer Structure2.3.3 The Boundary-Layer Response to a Rapid Pressure Variation; 2.4 Shock Waves and Boundary Layers: The Confrontation; 2.4.1 The Basic SBLI in Two-Dimensional Flows; 2.4.2 The Boundary-Layer-Shock-Pressure-Jump Competition; 2.5 Interactions without Separation: Weakly Interacting Flows; 2.5.1 The Incident-Reflecting Shock; Overall Flow Organisation; Shock Penetration in a Rotational Layer; 2.5.2 Ramp-Induced Shock; 2.5.3 Normal Shock and Transonic Interactions; 2.5.4 Upstream Influence Scaling. | |
| 505 | 8 | |a 2.6 Interaction Producing Boundary-Layer Separation: Strongly Interacting Flows2.6.1 Separation Caused by an Incident Shock; Overall Flow Organisation; The Outer Inviscid-Flow Structure; 2.6.2 Ramp-Induced Separation; 2.6.3 Normal Shock-Induced Separation or Transonic Separation; 2.7 Separation in Supersonic-Flow and Free-Interaction Processes; 2.7.1 The Free-Interaction Theory; 2.7.2 Incipient Shock-Induced Separation in Turbulent Flow; 2.8 Transitional SBLIs; 2.9 Specific Features of Hypersonic Interactions; 2.9.1 Shock Pattern and Flowfield Organisation; 2.9.2 Wall-Temperature Effect. | |
| 505 | 8 | |a 2.9.3 Wall-Heat Transfer in Hypersonic Interactions2.9.4 Entropy-Layer Effect; 2.9.5 Real-Gas Effects on SBLI; 2.10 A Brief Consideration of Three-Dimensional Interacting Flows; 2.10.1 Separation in Three-Dimensional Flow; 2.10.2 Topology of a Three-Dimensional Interaction; 2.10.3 Reconsideration of Two-Dimensional Interaction; 2.11 Unsteady Aspects of Strong Interactions; 2.12 SBLI Control; 2.12.1 Mechanisms for Control Action; 2.12.2 Examination of Control Techniques; Active Control; Passive Control; Wall Contouring; 2.13 Concluding Remarks. | |
| 505 | 8 | |a Appendix A: Discontinuities in Supersonic Flow and the Rankine-Hugoniot Equations3 Transonic Shock Wave-Boundary- Layer Interactions; 3.1 Introduction to Transonic Interactions; 3.2 Applications of Transonic SBLIs and Associated Performance Losses; 3.2.1 Transonic Airfoils and Cascades; Shock Losses on Transonic Wings; 3.2.2 Supersonic Engine Intakes; 3.2.3 Internal Flows; 3.3 Normal SBLIs in Detail; 3.3.1 Attached-Flow Interaction; Region I (Upstream of Main Shock); Region II (Downstream of Main Shock); Inflow-Shape-Factor Effects; 3.3.2 The Onset of Shock-Induced Separation. | |
| 546 | |a English. | ||
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Shock waves. | |
| 650 | 0 | |a Boundary layer. | |
| 650 | 6 | |a Ondes de choc. | |
| 650 | 6 | |a Couche limite. | |
| 650 | 7 | |a TECHNOLOGY & ENGINEERING |x Engineering (General) |2 bisacsh | |
| 650 | 7 | |a TRANSPORTATION |x Aviation |x General. |2 bisacsh | |
| 650 | 7 | |a Boundary layer |2 fast | |
| 650 | 7 | |a Shock waves |2 fast | |
| 700 | 1 | |a Babinsky, Holger. | |
| 700 | 1 | |a Harvey, John |q (John K.) | |
| 776 | 0 | 8 | |i Print version: |t Shock wave-boundary-layer interactions. |d Cambridge ; New York : Cambridge University Press, 2011 |z 9780521848527 |w (DLC) 2011001978 |w (OCoLC)701672464 |
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