Basics of aerothermodynamics:
Saved in:
| Main Author: | |
|---|---|
| Format: | Book |
| Language: | English |
| Published: |
Cham ; Heidelberg ; New York ; Dordrecht ; London
Springer
[2015]
|
| Edition: | Second, revised edition |
| Subjects: | |
| Online Access: | Inhaltsverzeichnis |
| Physical Description: | XVII, 446 Seiten Illustrationen, Diagramme 24 cm |
| ISBN: | 9783319143729 9783319330402 |
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MARC
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| 245 | 1 | 0 | |a Basics of aerothermodynamics |c Ernst Heinrich Hirschel |
| 250 | |a Second, revised edition | ||
| 264 | 1 | |a Cham ; Heidelberg ; New York ; Dordrecht ; London |b Springer |c [2015] | |
| 264 | 4 | |c © 2015 | |
| 300 | |a XVII, 446 Seiten |b Illustrationen, Diagramme |c 24 cm | ||
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| 650 | 4 | |a Engineering | |
| 650 | 4 | |a Thermodynamics | |
| 650 | 4 | |a Vibration | |
| 650 | 4 | |a Hydraulic engineering | |
| 650 | 4 | |a Astronautics | |
| 650 | 4 | |a Aerospace Technology and Astronautics | |
| 650 | 4 | |a Fluid- and Aerodynamics | |
| 650 | 4 | |a Engineering Thermodynamics, Heat and Mass Transfer | |
| 650 | 4 | |a Engineering Fluid Dynamics | |
| 650 | 4 | |a Vibration, Dynamical Systems, Control | |
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Record in the Search Index
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| adam_text | Titel: Basics of aerothermodynamics
Autor: Hirschel, Ernst Heinrich
Jahr: 2015
Table of Contents
Introduction.......................................... 1
1.1 Classes of Hypersonic Vehicles and Their
Aerothermodynamic Peculiarities......................... 1
1.2 RV-Type and CAV-Type Flight Vehicles as Reference
Vehicles............................................... 5
1.3 The Tasks of Aerothermodynamics ....................... 11
1.4 The Thermal State of the Surface and Thermal Surface
Effects................................................ 13
1.5 Unsteady Flight and Steady Aerothermodynamics?......... 17
1.6 Scope and Content of the Book .......................... 18
References................................................. 20
The Flight Environment............................... 23
2.1 The Earth Atmosphere.................................. 23
2.2 Atmospheric Properties and Models....................... 28
2.3 Flow Regimes.......................................... 30
2.4 Problems.............................................. 34
References................................................. 34
Thermal Radiation Cooling of External Vehicle
Surfaces.............................................. 37
3.1 Definitions............................................. 37
3.2 The Radiation-Adiabatic Vehicle Surface.................. 41
3.2.1 Introduction: Surface Radiation Cooling............. 41
3.2.2 Local Analysis of Radiation Cooling................ 43
3.2.3 The Radiation-Adiabatic Surface and Reality........ 47
3.2.4 Qualitative Behavior of the Radiation-Adiabatic
Temperature on Real Configurations................ 50
3.2.5 Non-convex Effects............................... 53
3.2.6 Scaling of the Radiation-Adiabatic Temperature...... 57
3.2.7 Some Parametric Considerations of the
Radiation-Adiabatic Temperature.................. 59
3.3 Case Study: The Thermal State of the Surface of the Blunt
Delta Wing............................................ 63
3.3.1 Configuration and Computation Cases.............. 63
XIV Table of Contents
3.3.2 Topology of the Computnd Skin-Friction and Velocity
Fields........................................... 63
3.3.3 The Computed Radiation-Adiabatic Temperature
Field ........................................... 67
3.4 Sunmiary of the Results of the Chapter in View
of Flight-Vehicle Design................................. 72
3.5 Problems.............................................. 73
References................................................. 74
4 Transport of Momentum, Energy and Mass ............. 77
4.1 Transport Phenomena................................... 78
4.2 Transport Properties.................................... 82
4.2.1 Introduction..................................... 82
4.2.2 Viscosity........................................ 83
4.2.3 Thermal Conductivity ............................ 84
4.2.4 Mass Diffusivity.................................. 86
4.2.5 Computation Models ............................. 88
4.3 Equations of Motion, Initial Conditions, Boundary
Conditions, and Similarity Parameters .................... 90
4.3.1 Transport of Momentum.......................... 90
4.3.2 Transport of Energy.............................. 95
4.3.3 Transport of Mass................................102
4.4 Remarks on Similarity Parameters........................106
4.5 Problems..............................................107
References.................................................107
5 Real-Gas Aerothermodynamic Phenomena.............. 111
5.1 Van der Waals Effects................................... 112
5.2 High-Temperature Real-Gas Effects....................... 114
5.3 Dissociation and Recombination.......................... 118
5.4 Thermal and Chemical Rate Processes.................... 119
5.5 Rate Effects, Two Examples............................. 123
5.5.1 Shock-Wave Flow in the Presence of Rate Effects..... 123
5.5.2 Nozzle Flow in a Hot Ground-Simulation Facility . . . 126
5.6 Surface Catalytic Recombination......................... 131
5.7 A Few Remarks on Simulation Issues ..................... 138
5.8 Computation Models.................................... 139
5.9 Problems.............................................. 140
References................................................. 141
6 Inviscid Aerothermodynamic Phenomena...............145
6.1 Hypersonic Flight Vehicles and Shock Waves...............146
6.2 One-Dimensional Shock-Free Flow........................152
6.3 Shock Waves...........................................156
6.3.1 The Normal Shock Wave..........................156
Table of Contents XV
6.3.2 The Oblique Shock Wave..........................163
6.3.3 Treatment of Shock Waves in Computational
Methods ........................................173
6.4 Blunt-Body Flow.......................................176
6.4.1 Bow-Shock Stand-Off Distance at a Blunt Body......176
6.4.2 The Entropy Layer at a Blunt Body................182
6.5 Supersonic Turning: Prandtl-Meyer Expansion and
Isentropic Compression..................................188
6.6 The Change of the Unit Reynolds Number across Shock
Waves ................................................192
6.7 Newton Flow ..........................................196
6.7.1 Basics of Newton Flow............................196
6.7.2 Modification Schemes, Application Aspects..........199
6.8 The Mach-Number Independence Principle of Oswatitsch . . . 204
6.9 Problems..............................................210
References.................................................211
7 Attached High-Speed Viscous Flow.....................215
7.1 Attached Viscous Flow..................................216
7.1.1 Attached Viscous Flow as Flow Phenomenon........216
7.1.2 Some Properties of Three-Dimensional Attached
Viscous Flow ....................................217
7.1.3 Boundary-Layer Equations ........................218
7.1.4 Global Characteristic Properties of Attached Viscous
Flow............................................227
7.1.5 Wall Compatibility Conditions.....................229
7.1.6 The Reference Temperature/Enthalpy Method for
Compressible Boundary Layers.....................233
7.1.7 Equations of Motion for Hypersonic Attached Viscous
Flow............................................236
7.2 Basic Properties of Attached Viscous Flow.................240
7.2.1 Boundary-Layer Thicknesses and Integral
Parameters......................................240
7.2.2 Boundary-Layer Thickness at Stagnation Points and
Attachment Lines................................254
7.2.3 Wall Shear Stress at Fiat Surface Portions...........256
7.2.4 Wall Shear Stress at Attachment Lines..............260
7.2.5 The Thermal State of Fiat Surface Portions .........263
7.2.6 The Thermal State of Stagnation Points and
Attachment Lines................................265
7.3 Case Study: Wall Temperature and Skin Friction at the
SÄNGER Forebody.....................................269
7.4 Problems..............................................275
References.................................................276
XVI Table of Contents
8 Laminar-Turbulent Transition and Turbulence in
High-Speed Viscous Flow..............................279
8.1 Laminar-Turbulent Transition as Hypersonic Flow
Phenomenon...........................................282
8.1.1 Some Basic Observations..........................283
8.1.2 Outline of Stability Theory........................286
8.1.3 Inviscid Stability Theory and the Point-of-Inflection
Criterion........................................289
8.1.4 The Influence of the Mach Number and the Thermal
State of the Surface...............................292
8.2 Real Flight-Vehicle Effects...............................295
8.2.1 Cone versus Flat-Plate Boundary-Layer Transition . . . 296
8.2.2 Effect of Nose Bluntness—Entropy-Layer Instability . . 297
8.2.3 Attachment-Line Instability .......................298
8.2.4 Attachment-Line Contamination ...................299
8.2.5 Effect of Three-Dimensional Flow—Cross-Flow
Instability.......................................301
8.2.6 Effect of Shock/Boundary-Layer Interaction .........302
8.2.7 High-Temperature Real-Gas Effects.................303
8.2.8 Görtier Instability................................303
8.2.9 Relaminarization.................................306
8.3 Receptivity Issues ......................................307
8.3.1 Surface Properties................................307
8.3.2 Free-Stream Disturbanccs: The Environment.........310
8.4 Prediction of Stability/Instability and Transition in
High-Speed Flows ......................................313
8.4.1 Stability/Instability Theory and Methods ...........313
8.4.2 Transition Models and Criteria.....................315
8.4.3 Concluding Remarks..............................319
8.5 Turbulence Modeling for High-Speed Flows................320
References.................................................323
9 Strong Interaction Phenomena.........................333
9.1 Flow Separation........................................334
9.2 Shock/Boundary-Layer Interaction Phenomena.............341
9.2.1 Ramp-Type (Edney Type VI and V) Interaction.....342
9.2.2 Nose/Leading-Edge-type (Edney Type IV and III)
Interaction ......................................351
9.3 Hypersonic Viscous Interaction...........................356
9.4 Low-Density Effects.....................................367
9.5 Problems..............................................374
References.................................................374
Table of Contents XVII
10 Viscous Thermal Surface Effects: Examples ............. 379
10.1 Introduction........................................... 379
10.2 Qualitative Considerations............................... 380
10.3 Examples in Foregoing Chapters.......................... 382
10.4 Boundary-Layer Thickness at a Heated Wall............... 383
10.5 Displacement Thickness at a Highly Cooled Wall........... 385
10.6 Cone-Flow Experiment: Amplification of the Second
Instability Mode by Cooling............................. 386
10.7 Reduction of the Turbulent Skin Friction with Side Effects ... 388
10.8 Fiat Plate/Ramp: Length of the Separation Zone........... 390
10.9 Generic Scramjet Inlet: The Shock-on-Lip Situation......... 394
lO.lOProblems.............................................. 396
References................................................. 397
11 Solution Guide and Solutions of the Problems...........399
Reference..................................................411
Appendix A: Governing Equations for Flow in General
Coordinates..........................................413
References.................................................416
Appendix B: Constants, Functions, SI Dimensions and
Conversions..........................................417
B.l Constants and Air Properties............................417
B.2 Dimensions and Conversions.............................418
References.................................................421
Appendix C: Symbols and Acronyms.........................423
Ol Latin Letters ..........................................423
C.2 Greek Letters..........................................425
C.3 Indices................................................427
C.3.1 Upper Indices....................................427
C.3.2 Lower Indices....................................427
C.4 Other Symbols.........................................429
C.5 Acronyms.............................................429
Permissions...................................................431
Name Index..................................................433
Subject Index ................................................439
|
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| author | Hirschel, Ernst Heinrich 1934- |
| author_GND | (DE-588)122980379 |
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| dewey-full | 629.1 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.1 |
| dewey-search | 629.1 |
| dewey-sort | 3629.1 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Physik Verkehr / Transport |
| edition | Second, revised edition |
| format | Book |
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| id | DE-604.BV042391805 |
| illustrated | Illustrated |
| indexdate | 2024-07-10T01:20:18Z |
| institution | BVB |
| isbn | 9783319143729 9783319330402 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-027827674 |
| oclc_num | 904447109 |
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| owner | DE-355 DE-BY-UBR DE-83 DE-210 DE-706 |
| owner_facet | DE-355 DE-BY-UBR DE-83 DE-210 DE-706 |
| physical | XVII, 446 Seiten Illustrationen, Diagramme 24 cm |
| publishDate | 2015 |
| publishDateSearch | 2015 |
| publishDateSort | 2015 |
| publisher | Springer |
| record_format | marc |
| spelling | Hirschel, Ernst Heinrich 1934- Verfasser (DE-588)122980379 aut Basics of aerothermodynamics Ernst Heinrich Hirschel Second, revised edition Cham ; Heidelberg ; New York ; Dordrecht ; London Springer [2015] © 2015 XVII, 446 Seiten Illustrationen, Diagramme 24 cm txt rdacontent n rdamedia nc rdacarrier Engineering Thermodynamics Vibration Hydraulic engineering Astronautics Aerospace Technology and Astronautics Fluid- and Aerodynamics Engineering Thermodynamics, Heat and Mass Transfer Engineering Fluid Dynamics Vibration, Dynamical Systems, Control Ingenieurwissenschaften Aerothermodynamik (DE-588)4133168-0 gnd rswk-swf Aerothermodynamik (DE-588)4133168-0 s DE-604 Erscheint auch als Online-Ausgabe 978-3-319-14373-6 HBZ Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=027827674&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Hirschel, Ernst Heinrich 1934- Basics of aerothermodynamics Engineering Thermodynamics Vibration Hydraulic engineering Astronautics Aerospace Technology and Astronautics Fluid- and Aerodynamics Engineering Thermodynamics, Heat and Mass Transfer Engineering Fluid Dynamics Vibration, Dynamical Systems, Control Ingenieurwissenschaften Aerothermodynamik (DE-588)4133168-0 gnd |
| subject_GND | (DE-588)4133168-0 |
| title | Basics of aerothermodynamics |
| title_auth | Basics of aerothermodynamics |
| title_exact_search | Basics of aerothermodynamics |
| title_full | Basics of aerothermodynamics Ernst Heinrich Hirschel |
| title_fullStr | Basics of aerothermodynamics Ernst Heinrich Hirschel |
| title_full_unstemmed | Basics of aerothermodynamics Ernst Heinrich Hirschel |
| title_short | Basics of aerothermodynamics |
| title_sort | basics of aerothermodynamics |
| topic | Engineering Thermodynamics Vibration Hydraulic engineering Astronautics Aerospace Technology and Astronautics Fluid- and Aerodynamics Engineering Thermodynamics, Heat and Mass Transfer Engineering Fluid Dynamics Vibration, Dynamical Systems, Control Ingenieurwissenschaften Aerothermodynamik (DE-588)4133168-0 gnd |
| topic_facet | Engineering Thermodynamics Vibration Hydraulic engineering Astronautics Aerospace Technology and Astronautics Fluid- and Aerodynamics Engineering Thermodynamics, Heat and Mass Transfer Engineering Fluid Dynamics Vibration, Dynamical Systems, Control Ingenieurwissenschaften Aerothermodynamik |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=027827674&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT hirschelernstheinrich basicsofaerothermodynamics |