Gas dynamics
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Vorheriger Titel: | John, James E. A. Gas dynamics |
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1. Verfasser: | |
Format: | Buch |
Sprache: | English |
Veröffentlicht: |
Upper Saddle River, NJ
Pearson Prentice Hall
2006
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Ausgabe: | 3. ed. |
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adam_text | GAS DYNAMICS THIRD EDITION JAMES E. JOHN PRESIDENT, KETTERING UNIVERSITY
FLINT, MICHIGAN THEO G. KEITH DEPARTMENT OF MECHANICAL AND MANUFACTURING
ENGINEERING UNIVERSITY OF TOLEDO TOLEDO, OHIO PEARSON PRENTICE HALL
PEARSON EDUCATION INTERNATIONAL CONTENTS PREFACE XIII CHAPTER 1 BASIC
EQUATIONS OF COMPRESSIBLE FLOW 1 1.1 FLUIDS: LIQUIDS AND GASES 1 1.2
CONTINUUM 2 1.3 VISCOSITY AND THE BOUNDARY LAYER 3 1.4 EQUATIONS OF
MOTION 4 1.5 UNITS OF MEASUREMENT 4 1.6 EQUATION OF STATE 5 1.7
CONTROL-VOLUME APPROACH 8 1.8 CONSERVATION OF MASS 10 1.9 CONSERVATION
OF MOMENTUM 14 1.10 CONSERVATION OF ENERGY: THE FIRST LAW OF
THERMODYNAMICS 18 1.11 SECOND LAW OF THERMODYNAMICS 23 1.12
ONE-DIMENSIONAL FLOW 28 1.13 CHAPTER CAPSTONE APPLICATION: THE JET
EJECTOR 30 1.14 SUMMARY 34 1.15 REFERENCES 34 1.16 PROBLEMS 34 CHAPTER 2
WAVE PROPAGATION IN COMPRESSIBLE MEDIA 39 2.1 INTRODUCTION , 39 2.2 WAVE
PROPAGATION IN ELASTIC MEDIA 39 2.3 VELOCITY OF SOUND 41 2.4 SUBSONIC
AND SUPERSONIC FLOWS 51 2.5 MACH NUMBER 57 2.6 CHAPTER CAPSTONE
APPLICATION: THE SPEED OF SOUND IN A REAL GAS 58 2.7 SUMMARY 63 2.8
REFERENCES 64 2.9 PROBLEMS 64 VII VIII CONTENTS CHAPTER 3 ISENTROPIC
FLOW OF A PERFECT GAS 68 3.1 INTRODUCTION 68 3.2 EQUATIONS OF MOTION 69
3.3 SUBSONIC AND SUPERSONIC ISENTROPIC FLOW THROUGH A VARYING AREA
CHANNEL 72 3.4 STAGNATION PROPERTIES 74 3.5 ISENTROPIC FLOW IN A
CONVERGING NOZZLE 83 3.6 ISENTROPIC FLOW IN A CONVERGING-DIVERGING
NOZZLE 89 3.7 CHAPTER CAPSTONE APPLICATION: DEPRESSURIZATION OF A
STORAGE RESERVOIR OF FINITE SIZE 93 3.8 SUMMARY 101 3.9 REFERENCES 102
3.10 PROBLEMS 102 CHAPTER 4 STATIONARY NORMAL SHOCKWAVES 107 4.1
INTRODUCTION 107 4.2 FORMATION OF A NORMAL SHOCKWAVE 107 4.3 EQUATIONS
GOVERNING A STATIONARY NORMAL SHOCKWAVE 110 4.4 STATIONARY NORMAL
SHOCKWAVE IN A CONVERGING-DIVERGING NOZZLE 131 4.5 DETERMINING THE
LOCATION OF A STATIONARY NORMAL SHOCK IN A C-D NOZZLE 137 4.6
CONVERGING-DIVERGING SUPERSONIC DIFFUSER 139 4.7 CHAPTER CAPSTONE
APPLICATION: SUPERSONIC WIND TUNNELS 143 4.8 SUMMARY 149 4.9 REFERENCES
150 4.10 PROBLEMS 150 CHAPTER 5 MOVING NORMAL SHOCKWAVES 157 5.1
INTRODUCTION 157 5.2 MOVING NORMAL SHOCKWAVES 157 5.3 REFLECTED NORMAL
SHOCKWAVES 168 5.4 CHAPTER CAPSTONE APPLICATION: THE SHOCK TUBE (THE
RIEMANN PROBLEM) 173 5.5 SUMMARY 184 5.6 REFERENCES 184 5.7 PROBLEMS 185
CHAPTER 6 OBLIQUE SHOCKWAVES 189 6.1 INTRODUCTION 189 6.2 EQUATIONS OF
MOTION FOR A STRAIGHT OBLIQUE SHOCKWAVE 190 6.3 OBLIQUE-SHOCK
REFLECTIONS 210 6.4 CHAPTER CAPSTONE APPLICATION: THE INTERSECTION OF
TWO OBLIQUE SHOCKS 212 6.5 SUMMARY 224 6.6 REFERENCES 224 6.7 PROBLEMS
225 CONTENTS IX CHAPTER 7 PRANDTL-MEYER FLOW 229 7.1 INTRODUCTION 229
7.2 THERMODYNAMIC CONSIDERATIONS 229 7.3 GRADUAL COMPRESSIONS AND
EXPANSIONS 230 7.4 FLOW EQUATIONS FOR A PRANDTL-MEYER EXPANSION FAN 234
7.5 PRANDTL-MEYER FLOW IN A SMOOTH COMPRESSION 243 7.6 MAXIMUM TURNING
ANGLE FOR PRANDTL-MEYER FLOW 243 7.7 REFLECTIONS 244 7.8 CHAPTER
CAPSTONE APPLICATION: CONFLUENCE OF AN OBLIQUE SHOCK AND AN EXPANSION
FAN 245 7.9 SUMMARY 248 7.10 REFERENCES 249 7.11 PROBLEMS 249 CHAPTER 8
APPLICATIONS INVOLVING SHOCKS AND EXPANSION FANS 254 8.1 INTRODUCTION
254 8.2 SUPERSONIC OBLIQUE-SHOCK DIFFUSER 254 8.3 EXIT FLOW FOR
UNDEREXPANDED AND OVEREXPANDED SUPERSONIC NOZZLES 260 8.4 PLUG NOZZLE
262 8.5 SUPERSONIC AIRFOILS 270 8.6 CHAPTER CAPSTONE APPLICATION:
SURFACE PRESSURE DISTRIBUTION ON A BODY IN A HIGH-MACH-NUMBER FLOW 277
8.7 SUMMARY 279 8.8 REFERENCES 279 8.9 PROBLEMS 280 CHAPTER 9 FLOW WITH
FRICTION 283 9.1 INTRODUCTION 283 9.2 FANNO LINE FLOW 284 9.3 WORKING
RELATIONS FOR FANNO FLOW 289 9.4 FLOW THROUGH A NOZZLE AND CONSTANT-AREA
DUCT IN SERIES 298 9.5 A NONITERATIVE METHOD TO LOCATE A NORMAL SHOCK IN
A CONSTANT-AREA DUCT WITH FRICTION THAT IS CONNECTED TO RESERVOIR BY A
C-D NOZZLE 304 9.6 ADIABATIC FLOW WITH FRICTION AND AREA CHANGE 310 9.7
CHAPTER CAPSTONE APPLICATION: NUMERICAL SOLUTION OF THE ORDINARY
DIFFERENTIAL EQUATION FOR ADIABATIC FLOW WITH FRICTION AND AREA CHANGE
314 9.8 SUMMARY 330 9.9 REFERENCES 330 9.10 PROBLEMS 331 CHAPTER 10 FLOW
WITH HEAT ADDITION OR HEAT LOSS 337 10.1 INTRODUCTION 337 10.2 RAYLEIGH
LINE FLOW 338 10.3 NORMAL SHOCK ON RAYLEIGH AND FANNO LINE T-S DIAGRAMS
355 X CONTENTS 10.4 FLOWS WITH HEAT ADDITION AND AREA CHANGE 355 10.5
FLOWS WITH FRICTION AND HEAT ADDITION 360 10.6 CHAPTER CAPSTONE
APPLICATION: ISOTHERMAL FLOW 365 10.7 SUMMARY 370 10.8 REFERENCES 370
10.9 PROBLEMS 371 CHAPTER 11 EQUATIONS OF MOTION FOR MULTIDIMENSIONAL
FLOW 375 11.1 INTRODUCTION 375 11.2 CONTINUITY EQUATION 376 11.3
MOMENTUM EQUATION 379 11.4 ENERGY EQUATION 382 11.5 CONSERVATION FORM OF
THE GOVERNING EQUATIONS 387 11.6 IRROTATIONAL FLOW 388 11.7 CROCCO S
EQUATION 392 11.8 VELOCITY POTENTIAL 394 11.9 EQUATIONS OF MOTION IN
TERMS OF VELOCITY POTENTIAL 395 11.10 SUMMARY 403 11.11 REFERENCES 403
11.12 PROBLEMS 404 CHAPTER 12 EXACT SOLUTIONS 406 12.1 INTRODUCTION 406
12.2 SIMPLE HOMENTROPIC FLOWS 407 12.3 THE HODOGRAPH TRANSFORMATION 421
12.4 FLOWS AROUND CORNERS 431 12.5 CONICAL FLOW 439 12.6 SUMMARY 449
12.7 REFERENCES 449 12.8 PROBLEMS 450 CHAPTER 13 LINEARIZED FLOWS 453
13.1 INTRODUCTION 453 13.2 LINEARIZATION OF THE POTENTIAL EQUATION 453
13.3 SUBSONIC FLOW OVER A WAVY WALL 459 13.4 SIMILARITY LAWS FOR
SUBSONIC FLOW - 464 13.5 SUPERSONIC FLOW OVER A WAVY WALL 474 13.6 THIN
AIRFOILS IN SUPERSONIC FLOW 481 13.7 SUMMARY 489 13.8 REFERENCES 489
13.9 PROBLEMS 490 CHAPTER 14 CHARACTERISTICS 494 14.1 INTRODUCTION 494
14.2 PROPERTIES OF CHARACTERISTICS 495 CONTENTS XI 14.3 THEORY OF
CHARACTERISTICS 498 14.4 CALCULATION PROCEDURES 522 14.5
SUPERSONIC-NOZZLE DESIGN 540 14.6 SUMMARY 545 14.7 REFERENCES 546 14.8
PROBLEMS 547 CHAPTER 15 MEASUREMENTS IN COMPRESSIBLE FLOW 553 15.1
INTRODUCTION 553 15.2 PRESSURE MEASUREMENT 553 15.3 TEMPERATURE
MEASUREMENT 561 15.4 VELOCITY MEASUREMENT 570 15.5 DENSITY AND OPTICAL
METHODS OF MEASUREMENT 580 15.6 FLOW RATE MEASUREMENT 596 15.7 SUMMARY
602 15.8 REFERENCES 602 15.9 PROBLEMS 604 APPENDIX A ONE-DIMENSIONAL
EQUATIONS OF GAS DYNAMICS FOR USE IN SPREADSHEET PROGRAMS 606 A.I
ISENTROPIC FLOW 607 A.2 NORMAL SHOCKWAVES 609 A.3 OBLIQUE SHOCKWAVES 612
A.4 PRANDTL-MEYER FLOW 616 A.5 FANNO FLOW 618 A. 6 RAYLEIGH FLOW 620 A.7
ISOTHERMAL FLOW 623 APPENDIX B ISENTROPIC FLOW TABLES , 628 APPENDIX C
NORMAL SHOCK-TABLES 632 APPENDIX D OBLIQUE-SHOCK CHARTS 638 APPENDIX E
PRANDTL-MEYER FUNCTIONS 645 APPENDIX F FANNO LINE FLOW 648 APPENDIX G
RAYLEIGH LINE FLOW 652 APPENDIX H PHYSICAL PROPERTIES OF GASES 656
APPENDIX I STANDARD ATMOSPHERE 660 APPENDIX J CONVERSION FACTORS 663
INDEX 665
|
adam_txt |
GAS DYNAMICS THIRD EDITION JAMES E. JOHN PRESIDENT, KETTERING UNIVERSITY
FLINT, MICHIGAN THEO G. KEITH DEPARTMENT OF MECHANICAL AND MANUFACTURING
ENGINEERING UNIVERSITY OF TOLEDO TOLEDO, OHIO PEARSON PRENTICE HALL
PEARSON EDUCATION INTERNATIONAL CONTENTS PREFACE XIII CHAPTER 1 BASIC
EQUATIONS OF COMPRESSIBLE FLOW 1 1.1 FLUIDS: LIQUIDS AND GASES 1 1.2
CONTINUUM 2 1.3 VISCOSITY AND THE BOUNDARY LAYER 3 1.4 EQUATIONS OF
MOTION 4 1.5 UNITS OF MEASUREMENT 4 1.6 EQUATION OF STATE 5 1.7
CONTROL-VOLUME APPROACH 8 1.8 CONSERVATION OF MASS 10 1.9 CONSERVATION
OF MOMENTUM 14 1.10 CONSERVATION OF ENERGY: THE FIRST LAW OF
THERMODYNAMICS 18 1.11 SECOND LAW OF THERMODYNAMICS 23 1.12
ONE-DIMENSIONAL FLOW 28 1.13 CHAPTER CAPSTONE APPLICATION: THE JET
EJECTOR 30 1.14 SUMMARY 34 1.15 REFERENCES 34 1.16 PROBLEMS 34 CHAPTER 2
WAVE PROPAGATION IN COMPRESSIBLE MEDIA 39 2.1 INTRODUCTION , 39 2.2 WAVE
PROPAGATION IN ELASTIC MEDIA 39 2.3 VELOCITY OF SOUND 41 2.4 SUBSONIC
AND SUPERSONIC FLOWS 51 2.5 MACH NUMBER 57 2.6 CHAPTER CAPSTONE
APPLICATION: THE SPEED OF SOUND IN A REAL GAS 58 2.7 SUMMARY 63 2.8
REFERENCES 64 2.9 PROBLEMS 64 VII VIII CONTENTS CHAPTER 3 ISENTROPIC
FLOW OF A PERFECT GAS 68 3.1 INTRODUCTION 68 3.2 EQUATIONS OF MOTION 69
3.3 SUBSONIC AND SUPERSONIC ISENTROPIC FLOW THROUGH A VARYING AREA
CHANNEL 72 3.4 STAGNATION PROPERTIES 74 3.5 ISENTROPIC FLOW IN A
CONVERGING NOZZLE 83 3.6 ISENTROPIC FLOW IN A CONVERGING-DIVERGING
NOZZLE 89 3.7 CHAPTER CAPSTONE APPLICATION: DEPRESSURIZATION OF A
STORAGE RESERVOIR OF FINITE SIZE 93 3.8 SUMMARY 101 3.9 REFERENCES 102
3.10 PROBLEMS 102 CHAPTER 4 STATIONARY NORMAL SHOCKWAVES 107 4.1
INTRODUCTION 107 4.2 FORMATION OF A NORMAL SHOCKWAVE 107 4.3 EQUATIONS
GOVERNING A STATIONARY NORMAL SHOCKWAVE 110 4.4 STATIONARY NORMAL
SHOCKWAVE IN A CONVERGING-DIVERGING NOZZLE 131 4.5 DETERMINING THE
LOCATION OF A STATIONARY NORMAL SHOCK IN A C-D NOZZLE 137 4.6
CONVERGING-DIVERGING SUPERSONIC DIFFUSER 139 4.7 CHAPTER CAPSTONE
APPLICATION: SUPERSONIC WIND TUNNELS 143 4.8 SUMMARY 149 4.9 REFERENCES
150 4.10 PROBLEMS 150 CHAPTER 5 MOVING NORMAL SHOCKWAVES 157 5.1
INTRODUCTION 157 5.2 MOVING NORMAL SHOCKWAVES 157 5.3 REFLECTED NORMAL
SHOCKWAVES 168 5.4 CHAPTER CAPSTONE APPLICATION: THE SHOCK TUBE (THE
RIEMANN PROBLEM) 173 5.5 SUMMARY 184 5.6 REFERENCES 184 5.7 PROBLEMS 185
CHAPTER 6 OBLIQUE SHOCKWAVES 189 6.1 INTRODUCTION 189 6.2 EQUATIONS OF
MOTION FOR A STRAIGHT OBLIQUE SHOCKWAVE 190 6.3 OBLIQUE-SHOCK
REFLECTIONS 210 6.4 CHAPTER CAPSTONE APPLICATION: THE INTERSECTION OF
TWO OBLIQUE SHOCKS 212 6.5 SUMMARY 224 6.6 REFERENCES 224 6.7 PROBLEMS
225 CONTENTS IX CHAPTER 7 PRANDTL-MEYER FLOW 229 7.1 INTRODUCTION 229
7.2 THERMODYNAMIC CONSIDERATIONS 229 7.3 GRADUAL COMPRESSIONS AND
EXPANSIONS 230 7.4 FLOW EQUATIONS FOR A PRANDTL-MEYER EXPANSION FAN 234
7.5 PRANDTL-MEYER FLOW IN A SMOOTH COMPRESSION 243 7.6 MAXIMUM TURNING
ANGLE FOR PRANDTL-MEYER FLOW 243 7.7 REFLECTIONS 244 7.8 CHAPTER
CAPSTONE APPLICATION: CONFLUENCE OF AN OBLIQUE SHOCK AND AN EXPANSION
FAN 245 7.9 SUMMARY 248 7.10 REFERENCES 249 7.11 PROBLEMS 249 CHAPTER 8
APPLICATIONS INVOLVING SHOCKS AND EXPANSION FANS 254 8.1 INTRODUCTION
254 8.2 SUPERSONIC OBLIQUE-SHOCK DIFFUSER 254 8.3 EXIT FLOW FOR
UNDEREXPANDED AND OVEREXPANDED SUPERSONIC NOZZLES 260 8.4 PLUG NOZZLE
262 8.5 SUPERSONIC AIRFOILS 270 8.6 CHAPTER CAPSTONE APPLICATION:
SURFACE PRESSURE DISTRIBUTION ON A BODY IN A HIGH-MACH-NUMBER FLOW 277
8.7 SUMMARY 279 8.8 REFERENCES 279 8.9 PROBLEMS 280 CHAPTER 9 FLOW WITH
FRICTION 283 9.1 INTRODUCTION 283 9.2 FANNO LINE FLOW 284 9.3 WORKING
RELATIONS FOR FANNO FLOW 289 9.4 FLOW THROUGH A NOZZLE AND CONSTANT-AREA
DUCT IN SERIES 298 9.5 A NONITERATIVE METHOD TO LOCATE A NORMAL SHOCK IN
A CONSTANT-AREA DUCT WITH FRICTION THAT IS CONNECTED TO RESERVOIR BY A
C-D NOZZLE 304 9.6 ADIABATIC FLOW WITH FRICTION AND AREA CHANGE 310 9.7
CHAPTER CAPSTONE APPLICATION: NUMERICAL SOLUTION OF THE ORDINARY
DIFFERENTIAL EQUATION FOR ADIABATIC FLOW WITH FRICTION AND AREA CHANGE
314 9.8 SUMMARY 330 9.9 REFERENCES 330 9.10 PROBLEMS 331 CHAPTER 10 FLOW
WITH HEAT ADDITION OR HEAT LOSS 337 10.1 INTRODUCTION 337 10.2 RAYLEIGH
LINE FLOW 338 10.3 NORMAL SHOCK ON RAYLEIGH AND FANNO LINE T-S DIAGRAMS
355 X CONTENTS 10.4 FLOWS WITH HEAT ADDITION AND AREA CHANGE 355 10.5
FLOWS WITH FRICTION AND HEAT ADDITION 360 10.6 CHAPTER CAPSTONE
APPLICATION: ISOTHERMAL FLOW 365 10.7 SUMMARY 370 10.8 REFERENCES 370
10.9 PROBLEMS 371 CHAPTER 11 EQUATIONS OF MOTION FOR MULTIDIMENSIONAL
FLOW 375 11.1 INTRODUCTION 375 11.2 CONTINUITY EQUATION 376 11.3
MOMENTUM EQUATION 379 11.4 ENERGY EQUATION 382 11.5 CONSERVATION FORM OF
THE GOVERNING EQUATIONS 387 11.6 IRROTATIONAL FLOW 388 11.7 CROCCO'S
EQUATION 392 11.8 VELOCITY POTENTIAL 394 11.9 EQUATIONS OF MOTION IN
TERMS OF VELOCITY POTENTIAL 395 11.10 SUMMARY 403 11.11 REFERENCES 403
11.12 PROBLEMS 404 CHAPTER 12 EXACT SOLUTIONS 406 12.1 INTRODUCTION 406
12.2 SIMPLE HOMENTROPIC FLOWS 407 12.3 THE HODOGRAPH TRANSFORMATION 421
12.4 FLOWS AROUND CORNERS 431 12.5 CONICAL FLOW 439 12.6 SUMMARY 449
12.7 REFERENCES 449 12.8 PROBLEMS 450 CHAPTER 13 LINEARIZED FLOWS 453
13.1 INTRODUCTION 453 13.2 LINEARIZATION OF THE POTENTIAL EQUATION 453
13.3 SUBSONIC FLOW OVER A WAVY WALL 459 13.4 SIMILARITY LAWS FOR
SUBSONIC FLOW - 464 13.5 SUPERSONIC FLOW OVER A WAVY WALL 474 13.6 THIN
AIRFOILS IN SUPERSONIC FLOW 481 13.7 SUMMARY 489 13.8 REFERENCES 489
13.9 PROBLEMS 490 CHAPTER 14 CHARACTERISTICS 494 14.1 INTRODUCTION 494
14.2 PROPERTIES OF CHARACTERISTICS 495 CONTENTS XI 14.3 THEORY OF
CHARACTERISTICS 498 14.4 CALCULATION PROCEDURES 522 14.5
SUPERSONIC-NOZZLE DESIGN 540 14.6 SUMMARY 545 14.7 REFERENCES 546 14.8
PROBLEMS 547 CHAPTER 15 MEASUREMENTS IN COMPRESSIBLE FLOW 553 15.1
INTRODUCTION 553 15.2 PRESSURE MEASUREMENT 553 15.3 TEMPERATURE
MEASUREMENT 561 15.4 VELOCITY MEASUREMENT 570 15.5 DENSITY AND OPTICAL
METHODS OF MEASUREMENT 580 15.6 FLOW RATE MEASUREMENT 596 15.7 SUMMARY
602 15.8 REFERENCES 602 15.9 PROBLEMS 604 APPENDIX A ONE-DIMENSIONAL
EQUATIONS OF GAS DYNAMICS FOR USE IN SPREADSHEET PROGRAMS 606 A.I
ISENTROPIC FLOW 607 A.2 NORMAL SHOCKWAVES 609 A.3 OBLIQUE SHOCKWAVES 612
A.4 PRANDTL-MEYER FLOW 616 A.5 FANNO FLOW 618 A. 6 RAYLEIGH FLOW 620 A.7
ISOTHERMAL FLOW 623 APPENDIX B ISENTROPIC FLOW TABLES , 628 APPENDIX C
NORMAL SHOCK-TABLES 632 APPENDIX D OBLIQUE-SHOCK CHARTS 638 APPENDIX E
PRANDTL-MEYER FUNCTIONS '" 645 APPENDIX F FANNO LINE FLOW 648 APPENDIX G
RAYLEIGH LINE FLOW 652 APPENDIX H PHYSICAL PROPERTIES OF GASES 656
APPENDIX I STANDARD ATMOSPHERE 660 APPENDIX J CONVERSION FACTORS 663
INDEX 665 |
any_adam_object | 1 |
any_adam_object_boolean | 1 |
author | John, James E. |
author_facet | John, James E. |
author_role | aut |
author_sort | John, James E. |
author_variant | j e j je jej |
building | Verbundindex |
bvnumber | BV021496964 |
callnumber-first | Q - Science |
callnumber-label | QC168 |
callnumber-raw | QC168 |
callnumber-search | QC168 |
callnumber-sort | QC 3168 |
callnumber-subject | QC - Physics |
classification_rvk | UG 1300 |
classification_tum | MTA 390f |
ctrlnum | (OCoLC)62133814 (DE-599)BVBBV021496964 |
dewey-full | 533/.2 |
dewey-hundreds | 500 - Natural sciences and mathematics |
dewey-ones | 533 - Pneumatics (Gas mechanics) |
dewey-raw | 533/.2 |
dewey-search | 533/.2 |
dewey-sort | 3533 12 |
dewey-tens | 530 - Physics |
discipline | Physik |
discipline_str_mv | Physik |
edition | 3. ed. |
format | Book |
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genre | (DE-588)4123623-3 Lehrbuch gnd-content |
genre_facet | Lehrbuch |
id | DE-604.BV021496964 |
illustrated | Illustrated |
index_date | 2024-07-02T14:14:19Z |
indexdate | 2024-11-25T17:26:05Z |
institution | BVB |
isbn | 0131206680 |
language | English |
lccn | 2005054998 |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-014713728 |
oclc_num | 62133814 |
open_access_boolean | |
owner | DE-703 DE-91G DE-BY-TUM DE-634 |
owner_facet | DE-703 DE-91G DE-BY-TUM DE-634 |
physical | XV, 672 S. Ill., graph. Darst. |
publishDate | 2006 |
publishDateSearch | 2006 |
publishDateSort | 2006 |
publisher | Pearson Prentice Hall |
record_format | marc |
spellingShingle | John, James E. Gas dynamics Gaz, Dynamique des - Manuels d'enseignement supérieur Gaz, Dynamique des ram Gas dynamics Gasdynamik (DE-588)4019339-1 gnd |
subject_GND | (DE-588)4019339-1 (DE-588)4123623-3 |
title | Gas dynamics |
title_auth | Gas dynamics |
title_exact_search | Gas dynamics |
title_exact_search_txtP | Gas dynamics |
title_full | Gas dynamics James E. John ; Theo G. Keith |
title_fullStr | Gas dynamics James E. John ; Theo G. Keith |
title_full_unstemmed | Gas dynamics James E. John ; Theo G. Keith |
title_old | John, James E. A. Gas dynamics |
title_short | Gas dynamics |
title_sort | gas dynamics |
topic | Gaz, Dynamique des - Manuels d'enseignement supérieur Gaz, Dynamique des ram Gas dynamics Gasdynamik (DE-588)4019339-1 gnd |
topic_facet | Gaz, Dynamique des - Manuels d'enseignement supérieur Gaz, Dynamique des Gas dynamics Gasdynamik Lehrbuch |
url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=014713728&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
work_keys_str_mv | AT johnjamese gasdynamics AT keiththeog gasdynamics |