High-Pressure Flows for Propulsion Applications. (Record no. 34210)
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| fixed length control field | 09189nam a22004813i 4500 |
| 001 - CONTROL NUMBER | |
| control field | EBC29191770 |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | MiAaPQ |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20240724115802.0 |
| 006 - FIXED-LENGTH DATA ELEMENTS--ADDITIONAL MATERIAL CHARACTERISTICS | |
| fixed length control field | m o d | |
| 007 - PHYSICAL DESCRIPTION FIXED FIELD--GENERAL INFORMATION | |
| fixed length control field | cr cnu|||||||| |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 240724s2020 xx o ||||0 eng d |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 9781624105814 |
| Qualifying information | (electronic bk.) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| Canceled/invalid ISBN | 9781624105807 |
| 035 ## - SYSTEM CONTROL NUMBER | |
| System control number | (MiAaPQ)EBC29191770 |
| 035 ## - SYSTEM CONTROL NUMBER | |
| System control number | (Au-PeEL)EBL29191770 |
| 035 ## - SYSTEM CONTROL NUMBER | |
| System control number | (OCoLC)1147706344 |
| 040 ## - CATALOGING SOURCE | |
| Original cataloging agency | MiAaPQ |
| Language of cataloging | eng |
| Description conventions | rda |
| -- | pn |
| Transcribing agency | MiAaPQ |
| Modifying agency | MiAaPQ |
| 050 #4 - LIBRARY OF CONGRESS CALL NUMBER | |
| Classification number | TL780 |
| 082 0# - DEWEY DECIMAL CLASSIFICATION NUMBER | |
| Classification number | 629.475 |
| 100 1# - MAIN ENTRY--PERSONAL NAME | |
| Personal name | Bellan, Josette. |
| 245 10 - TITLE STATEMENT | |
| Title | High-Pressure Flows for Propulsion Applications. |
| 250 ## - EDITION STATEMENT | |
| Edition statement | 1st ed. |
| 264 #1 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE | |
| Place of production, publication, distribution, manufacture | Reston : |
| Name of producer, publisher, distributor, manufacturer | American Institute of Aeronautics & Astronautics, |
| Date of production, publication, distribution, manufacture, or copyright notice | 2020. |
| 264 #4 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE | |
| Date of production, publication, distribution, manufacture, or copyright notice | ©2020. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Extent | 1 online resource (804 pages) |
| 336 ## - CONTENT TYPE | |
| Content type term | text |
| Content type code | txt |
| Source | rdacontent |
| 337 ## - MEDIA TYPE | |
| Media type term | computer |
| Media type code | c |
| Source | rdamedia |
| 338 ## - CARRIER TYPE | |
| Carrier type term | online resource |
| Carrier type code | cr |
| Source | rdacarrier |
| 490 1# - SERIES STATEMENT | |
| Series statement | Progress in Astronautics and Aeronautics Series ; |
| Volume/sequential designation | v.260 |
| 505 0# - FORMATTED CONTENTS NOTE | |
| Formatted contents note | Intro -- Title page -- Copyright -- Table of Contents -- Preface -- 1 Microgravity Research on Quasi-Steady and Unsteady Combustion of Fuel Droplet at High Pressures -- I. INTRODUCTION -- II. FUEL DROPLET EVAPORATION -- III. FUEL DROPLET COMBUSTION -- IV. CONCLUSIONS -- ACKNOWLEDGMENTS -- REFERENCES -- 2 Laboratory Experiments of High-Pressure Fluid Drops -- I. INTRODUCTION -- II. INTRODUCTION TO THERMODYNAMICS OF INTERFACES -- III. EXPERIMENTAL TEST RIG: A HIGH-PRESSURE APPARATUS FOR FALLING DROPLETS -- IV. OPTICAL TECHNIQUES: PROGRESS ON DROPLET CHARACTERIZATION AT HIGH PRESSURE -- V. RESULTS -- VI. ON THE LIMITS OF VLE FORMULATIONS -- VII. CONCLUSIONS -- ACKNOWLEDGMENTS -- REFERENCES -- 3 Optical Diagnostics for Sprays at High Pressure -- I. INTRODUCTION -- II. OPTICAL MEASUREMENTS AT HIGH PRESSURE AND TEMPERATURE -- III. WHITE-LIGHT IMAGING -- IV. LASER IMAGING -- V. TECHNIQUES THAT COULD POTENTIALLY BROADEN THE SCOPE OF MEASUREMENTS -- VI. OVERVIEW -- REFERENCES -- 4 Supercritical Coaxial Jet Disintegration -- NOMENCLATURE -- SUBSCRIPTS -- I. INTRODUCTION -- II. EXPERIMENTAL FACILITY -- III. WORKING FLUID AND EXPERIMENTAL TECHNIQUE -- IV. RESULTS -- V. CONCLUSIONS -- REFERENCES -- 5 High-Pressure Experiments Relevant to Rocket Propulsion -- I. INTRODUCTION -- II. BACKGROUND AND PAST EXPERIMENTS IN MODEL ROCKET COMBUSTORS -- III. MEASUREMENT AND DATA ANALYSIS OVERVIEW -- IV. MODAL DECOMPOSITION METHODS -- V. QUANTITATIVE OPTICAL COMPARISONS -- VI. SUMMARY AND CONCLUSIONS -- REFERENCES -- 6 Forced and Unforced Shear Coaxial Mixing and Combustion at Subcritical and Supercritical Pressures -- I. INTRODUCTION -- II. BACKGROUND: COAXIAL JET -- III. EXPERIMENTAL FACILITIES AND INSTRUMENTATION -- IV. RESULTS -- V. CONCLUSIONS -- REFERENCES -- 7 Measurement of Heat Transfer in Liquid Rocket Combustors -- NOMENCLATURE -- SUBSCRIPTS -- SUPERSCRIPTS. |
| 505 8# - FORMATTED CONTENTS NOTE | |
| Formatted contents note | I. INTRODUCTION -- II. HEAT-TRANSFER MEASUREMENT METHODOLOGIES -- III. EXAMPLES OF HEAT-FLUX MEASUREMENTS -- IV. DISCUSSION OF HEAT-FLUX MEASUREMENT APPROACHES -- REFERENCES -- 8 Characterization of Droplet Nucleation Inside Supercritical Ethylene Jets Using Small-Angle X-Ray Scattering Technique -- I. INTRODUCTION -- II. EXPERIMENTAL METHODS -- III. SMALL-ANGLE X-RAY SCATTERING -- IV. DATA REDUCTION -- V. RESULTS AND DISCUSSION -- VI. CONCLUSIONS -- ACKNOWLEDGMENTS -- REFERENCES -- 9 Empirical Fundamental Equations of State for Pure Fluids and Mixtures -- I. INTRODUCTION -- II. EQUATIONS OF STATE -- III. FITTING EQUATIONS OF STATE -- IV. PERFORMANCE OF EQUATIONS OF STATE AND FUTURE CHALLENGES -- V. CONCLUSION -- REFERENCES -- 10 Molecular Simulations to Research Supercritical Fuel Properties -- I. INTRODUCTION -- II. MOLECULAR APPROACH FOR RESEARCHING SUPERCRITICAL FLUIDS -- III. MC SIMULATIONS OF THE PHASE EQUILIBRIUM DIAGRAMS OF -- ALKANE/NITROGEN MIXTURES USING VARIOUS POTENTIALS -- IV. MD SIMULATIONS OF AN -- HEPTANE DROPLET VAPORIZING INTO NITROGEN AT VARIOUS AMBIENT TEMPERATURES AND PRESSURES -- ACKNOWLEDGMENT -- REFERENCES -- 11 Large Eddy Simulations of High-Pressure Jets: Effect of Subgrid-Scale Modeling -- I. INTRODUCTION -- II. GOVERNING EQUATIONS AND NUMERICAL METHOD -- III. NUMERICAL ASPECTS -- IV. CONFIGURATION, BOUNDARY CONDITIONS AND INITIAL CONDITIONS -- V. RESULTS AND DISCUSSION -- VI. SUMMARY AND CONCLUSIONS -- ACKNOWLEDGMENTS -- REFERENCES -- 12 High Pressure Flames with Multicomponent Transport -- I. INTRODUCTION -- II. NONIDEAL FLUIDS -- III. BINARY MIXING LAYERS -- IV. FREELY PROPAGATING PREMIXED FLAMES -- V. STRAINED FLAMES -- VI. TRANSCRITICAL DIFFUSION FLAMES -- VII. CONCLUSION -- REFERENCES -- 13 Large-Eddy Simulation of Cryogenic Jet Injection at Supercritical Pressures -- I. INTRODUCTION -- II. THERMODYNAMICS MODEL. |
| 505 8# - FORMATTED CONTENTS NOTE | |
| Formatted contents note | III. CRYOGENIC SINGLE-COMPONENT INJECTION AT SUPERCRITICAL PRESSURE -- IV. CRYOGENIC BINARY COMPONENT INJECTION AT SUPERCRITICAL PRESSURE -- V. CONCLUSION -- ACKNOWLEDGMENTS -- REFERENCES -- 14 Detailed Modeling of Supercritical Jets and Flames -- I. INTRODUCTION -- II. FLUID PROPERTIES IN SUPERCRITICAL ENVIRONMENTS -- III. KINETIC MODELS FOR HIGH-PRESSURE COMBUSTION -- IV. METHODOLOGY FOR ROBUST AND ACCURATE SIMULATIONS OF SUPERCRITICAL FLUIDS WITH LARGE DENSITY CONTRASTS -- V. ROBUST SOLVERS FOR STIFF CHEMISTRY -- VI. LES OF LOX/GH2 SHEAR-COAXIAL JET FLAME AT SUPERCRITICAL PRESSURE -- VII. CONCLUSIONS -- REFERENCES -- 15 Modeling and Simulations of High-Pressure Practical Flows -- I. INTRODUCTION -- II. NUMERICAL TOOLS FOR HIGH-PRESSURE REACTING FLOW SIMULATION -- III. COUPLING REAL-GAS TABULATED THERMOCHEMISTRY AND COMPRESSIBLE LES SOLVER -- IV. SIMULATION OF REACTING AND NONREACTING TURBULENT FLOWS -- V. CONCLUSION -- ACKNOWLEDGMENTS -- APPENDIX A. AEXPRESSION OF THE HEAT CAPACITY AT CONSTANT PRESSURE ( -- APPENDIX B. 2-D CONVECTION OF A MIXTURE FRACTION POCKET [MIXT] -- APPENDIX C. COUPLING THE REAL-GAS TABULATED THERMOCHEMISTRY WITH A LOW-MACH CODE -- REFERENCES -- 16 Large-Eddy Simulation of Liquid Injection and Combustion Processes in High-Pressure Systems -- I. INTRODUCTION -- II. GOVERNING EQUATIONS AND SUBMODEL FORMULATIONS -- III. RESULTS AND DISCUSSION -- IV. SUMMARY AND CONCLUSIONS -- ACKNOWLEDGMENTS -- APPENDIX A. THERMODYNAMIC DERIVATIVES AS FUNCTION OF COMPRESSIBILITY FACTOR FOR THE CUBIC EQUATIONS OF STATE -- APPENDIX B. DEPARTURE FUNCTIONS FOR CUBIC EQUATIONS OF STATE -- REFERENCES -- 17 Simulation of the High-Pressure Combustion Process in Diesel Engines -- NOMENCLATURE -- SUPERSCRIPT -- SUBSCRIPT -- I. INTRODUCTION -- II. DIESEL SPRAY MODEL -- III. GOVERNING EQUATIONS FOR THE FLUID PHASE -- IV. COMBUSTION MODEL. |
| 505 8# - FORMATTED CONTENTS NOTE | |
| Formatted contents note | V. CONSTANT-VOLUME COMBUSTION CHAMBER VALIDATIONS -- VI. DIESEL ENGINE SIMULATIONS -- VII. SUMMARY AND CONCLUSIONS -- ACKNOWLEDGMENTS -- REFERENCES -- Index. |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc. | High-pressure flows occur in nature, in industrial processes and in manufactured devices but not in human personal experience which is limited to atmospheric pressure. In nature, high-pressure flows are found in petroleum reservoirs, at ocean depths, and in the atmospheres of planets such as Venus. In industry, the enhanced solubility that occurs at high pressures is used to extract certain chemical species; for example, the solubility of caffeine in supercritical carbon dioxide enables production of decaffeinated coffee and tea. Manufactured devices such as diesel engines and liquid rocket engines operate at pressures well above atmospheric pressure. How mixtures of chemical species behave under high-pressure conditions is described by thermodynamics. However, because thermodynamics cannot describe flows, thermodynamics must be coupled to concepts of motion and transport in order to construct a physical description characterizing all relevant processes in high-pressure flows. The chapters in this book describe observations and modeling of high-pressure flows encountered in aeronautics and astronautics. They have been selected to present the current understanding of high-pressure flows. By editorial intent, agreement between authors on all aspects of the high-pressure field of research was not sought as it was felt that revealing where disagreement exists on specific aspects indicates where the new research opportunities are. Experimental, theoretical and numerical studies are all represented in the chapters. Fundamental investigations are presented first, followed by practical studies. |
| 588 ## - SOURCE OF DESCRIPTION NOTE | |
| Source of description note | Description based on publisher supplied metadata and other sources. |
| 590 ## - LOCAL NOTE (RLIN) | |
| Local note | Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries. |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | Propulsion systems. |
| 655 #4 - INDEX TERM--GENRE/FORM | |
| Genre/form data or focus term | Electronic books. |
| 776 08 - ADDITIONAL PHYSICAL FORM ENTRY | |
| Relationship information | Print version: |
| Main entry heading | Bellan, Josette |
| Title | High-Pressure Flows for Propulsion Applications |
| Place, publisher, and date of publication | Reston : American Institute of Aeronautics & Astronautics,c2020 |
| International Standard Book Number | 9781624105807 |
| 797 2# - LOCAL ADDED ENTRY--CORPORATE NAME (RLIN) | |
| Corporate name or jurisdiction name as entry element | ProQuest (Firm) |
| 830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE | |
| Uniform title | Progress in Astronautics and Aeronautics Series |
| 856 40 - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | <a href="https://ebookcentral.proquest.com/lib/orpp/detail.action?docID=29191770">https://ebookcentral.proquest.com/lib/orpp/detail.action?docID=29191770</a> |
| Public note | Click to View |
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