LEADER 04796nam 2200601 a 450 001 9910778544703321 005 20230617002421.0 010 $a1-60086-676-X 010 $a1-60086-457-0 010 $a1-61583-080-4 035 $a(CKB)1000000000810492 035 $a(EBL)3111642 035 $a(SSID)ssj0000072428 035 $a(PQKBManifestationID)11997368 035 $a(PQKBTitleCode)TC0000072428 035 $a(PQKBWorkID)10095789 035 $a(PQKB)11372656 035 $a(Au-PeEL)EBL3111642 035 $a(CaPaEBR)ebr10516747 035 $a(OCoLC)922979074 035 $a(MiAaPQ)EBC3111642 035 $a(EXLCZ)991000000000810492 100 $a20060111d2004 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 00$aLiquid rocket thrust chambers$b[electronic resource] $easpects of modeling, analysis, and design /$fedited by Vigor Yang ... [et al.] 210 $aReston, Va. $cAmerican Institute of Aeronautics and Astronautics, Inc.$dc2004 215 $a1 online resource (760 p.) 225 1 $aProgress in astronautics and aeronautics ;$vv. 200 300 $aDescription based upon print version of record. 311 $a1-56347-223-6 320 $aIncludes bibliographical references and indexes. 327 $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"" 327 $a""Engine Pressure Schedule""""Nozzle 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"" 327 $a""Nomenclature""""Introduction""; ""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"" 327 $a""Theory and Design of Gas-Liquid Jet Injectors""""Theory 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"" 327 $a""Dynamics of Liquid Rocket Injectors""""Linear 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"" 327 $a""Experimental and Theoretical Investigation at Atmospheric Pressure with Simulants"" 410 0$aProgress in astronautics and aeronautics ;$vv. 200. 606 $aLiquid propellants 615 0$aLiquid propellants. 676 $a662.6/66 701 $aYang$b Vigor$0322720 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910778544703321 996 $aLiquid rocket thrust chambers$93838052 997 $aUNINA