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|2 22
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|a UAMI
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| 245 |
0 |
0 |
|a Liquid rocket thrust chambers :
|b aspects of modeling, analysis, and design /
|c edited by Vigor Yang [and others].
|
| 260 |
|
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|a Reston, Va. :
|b American Institute of Aeronautics and Astronautics,
|c ©2004.
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| 300 |
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|a 1 online resource (xx, 725 pages, 16 unnumbered pages of plates) :
|b illustrations (some color)
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|a text
|b txt
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|a online resource
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1 |
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|a Progress in astronautics and aeronautics ;
|v v. 200
|
| 504 |
|
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|a Includes bibliographical references and indexes.
|
| 588 |
0 |
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|a Print version record.
|
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|3 Use copy
|f Restrictions unspecified
|2 star
|5 MiAaHDL
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|a Electronic reproduction.
|b [Place of publication not identified] :
|c HathiTrust Digital Library,
|d 2010.
|5 MiAaHDL
|
| 538 |
|
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|a Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.
|u http://purl.oclc.org/DLF/benchrepro0212
|5 MiAaHDL
|
| 583 |
1 |
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|a digitized
|c 2010
|h HathiTrust Digital Library
|l committed to preserve
|2 pda
|5 MiAaHDL
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| 505 |
0 |
|
|a Cover -- Title -- Copyright -- Table of Contents -- Preface -- Acknowledgments -- Chapter 1 Propellant Injection Systems and Processes -- Introduction -- Rocket Application Design Requirements -- Thrust Level and Operating Pressure -- Propellant Type -- Engine Cycle or Feed System -- Common Combustion Device Development Risks -- Combustion Instability -- Combustion Chamber Overheating and Burnout -- Injector Face Erosion -- Low Thrust Chamber Assembly Performance -- Unsafe Transients -- Injection System Design Considerations
|
| 505 |
8 |
|
|a Engine Pressure ScheduleNozzle Expansion Ratio -- Contraction Ratio -- Chamber Length -- Injection Element and Pattern -- Critical Combustion Processes -- Injector Manifold Distribution -- Injector Spray Atomization -- Propellant Droplet Vaporization -- Bipropellant Mixing -- Candidate Injectors for Liquid Rocket Applications -- Coaxial Jet Injectors -- Impinging Jet Injectors -- Parallel Jet (Showerhead) Injectors -- Injector Design Synthesis -- Conclusions and R e commendations -- References -- Chapter 2 Design and Dynamics of Jet and Swirl Injectors
|
| 505 |
8 |
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|a NomenclatureIntroduction -- Classification of Injectors and Methods of Mixture Formation -- Liquid Injectors -- Gas-Liquid Injectors -- Intensification of Propellant Atomization and Mixing in Liquid Injectors -- Intensification of Propellant Atomization and Mixing in Gas-Liquid Injectors -- Theory and Design of Liquid Monopropellant Jet Injectors -- Flow Characteristics -- Effect of Injector Configuration -- Flow Coefficient -- Design Procedure -- Theory and Design of Gaseous Monopropellant Jet Injectors -- Flow Characteristics -- Design Procedure
|
| 505 |
8 |
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|a Theory and Design of Gas-Liquid Jet InjectorsTheory and Design of Liquid Monopropellant Swirl Injectors -- Flow Characteristics of Ideal Swirl Injector -- Flow Characteristics of Real Swirl Injectors -- Effect of Viscosity on Injector Operation -- Design Procedure -- Theory and Design of Liquid Bipropellant Swirl Injectors -- Injectors with External Mixing -- Injectors with Internal Mixing -- Modulation of Liquid Spray Characteristics of Swirl Injectors -- Design of Gas Swirl Injectors -- Design Procedure -- Selection of Geometric Dimensions and Flow Parameters
|
| 505 |
8 |
|
|a Dynamics of Liquid Rocket InjectorsLinear Dynamics of Jet Injectors -- Linear Dynamics of Swirl Injectors -- Acknowledgments -- References -- Chapter 3 Atomization in Coaxial-Jet Injectors -- Nomenclature -- Introduction -- Phenomenological Description and Literature Review -- General Scheme of Jet Disintegration and Drop Formation -- Studies of Elementary Processes -- Numerical Simulations of the Atomization Process -- Derivation of Droplet Size Distribution Functions -- Investigations of Atomization in Shear Coaxial Injectors
|
| 546 |
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|a English.
|
| 590 |
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|a Knovel
|b ACADEMIC - Aerospace & Radar Technology
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| 650 |
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0 |
|a Liquid propellants.
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| 650 |
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6 |
|a Propergols liquides.
|
| 650 |
|
7 |
|a Liquid propellants
|2 fast
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| 700 |
1 |
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|a Yang, Vigor.
|
| 776 |
0 |
8 |
|i Print version:
|t Liquid rocket thrust chambers.
|d Reston, Va. : American Institute of Aeronautics and Astronautics, ©2004
|z 1563472236
|w (DLC) 2006270072
|w (OCoLC)57466123
|
| 830 |
|
0 |
|a Progress in astronautics and aeronautics ;
|v v. 200.
|
| 856 |
4 |
0 |
|u https://appknovel.uam.elogim.com/kn/resources/kpLRTCAMAA/toc
|z Texto completo
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