LEADER 00885nam0 22002771i 450 001 990007261980403321 005 20031023122722.0 035 $a000726198 035 $aFED01000726198 035 $a(Aleph)000726198FED01 035 $a000726198 100 $a20021021d--------km-y0itay50------ba 101 0 $aita 105 $ay---n---001yy 200 1 $a<>campagne Inglesi tra il 600 e 800$edal proprietario coltivatore al fittavolo capitalista$fa cura di Ambrosoli,M; 210 $aTorino$cRosemberg e Salier$d1985 215 $a320 pg$d24 cm 700 1$aAmbrosoli,$bMauro$0133154 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990007261980403321 951 $aXV F2 56$b2739$dXV F2 56 951 $aXV F2 56$b2739$eDipartimento Teoria Economica e Applicazioni$fdte 959 $aDTE 996 $aCampagne Inglesi tra il 600 e 800$9686176 997 $aUNINA LEADER 04473nam 2200517 450 001 9910830290403321 005 20230808193238.0 010 $a1-118-89005-1 010 $a1-118-89004-3 035 $a(CKB)3710000000685624 035 $a(EBL)4529684 035 $a(MiAaPQ)EBC4529684 035 $a(EXLCZ)993710000000685624 100 $a20160602h20162016 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $2rdacontent 182 $2rdamedia 183 $2rdacarrier 200 10$aInternal combustion processes of liquid rocket engines $emodeling and numerical simulations /$fZhen-Guo Wang 210 1$aSingapore :$cWiley,$d2016. 210 4$dİ2016 215 $a1 online resource (395 p.) 300 $aDescription based upon print version of record. 311 $a1-118-89003-5 311 $a1-118-89002-7 320 $aIncludes bibliographical references at the end of each chapters and index. 327 $aTitle Page ; Copyright Page ; Contents; Preface; Chapter 1 Introduction ; 1.1 Basic Configuration of Liquid Rocket Engines; 1.1.1 Propellant Feed System; 1.1.2 Thrust Chamber; 1.2 Internal Combustion Processes of Liquid Rocket Engines; 1.2.1 Start and Shutdown; 1.2.2 Combustion Process; 1.2.3 Performance Parameters in Working Process; 1.3 Characteristics and Development History of Numerical Simulation of the Combustion Process in Liquid Rocket Engines; 1.3.1 Benefits of Numerical Simulation of the Combustion Process in Liquid Rocket Engines 327 $a1.3.2 Main Contents of Numerical Simulations of Liquid Rocket Engine Operating Process1.3.3 Development of Numerical Simulations of Combustion Process in Liquid Rocket Engines; 1.4 Governing Equations of Chemical Fluid Dynamics; 1.5 Outline of this Book; References; Chapter 2 Physical Mechanism and Numerical Modeling of Liquid Propellant Atomization ; 2.1 Types and Functions of Injectors in a Liquid Rocket Engine; 2.2 Atomization Mechanism of Liquid Propellant; 2.2.1 Formation of Static Liquid Droplet; 2.2.2 Breakup of Cylindrical Liquid Jet; 2.2.3 Liquid Sheet Breakup 327 $a2.2.4 Droplet Secondary Breakup2.3 Characteristics of Atomization in Liquid Rocket Engines; 2.3.1 Distribution Function of the Droplet Size; 2.3.2 Mean Diameter and Characteristic Diameter; 2.3.3 Measurement of Spray Size Distribution; 2.4 Atomization Modeling for Liquid Rocket Engine Atomizers; 2.4.1 Straight-flow Injector; 2.4.2 Centrifugal Injector; 2.4.3 Impinging-stream Injectors; 2.4.4 Coaxial Shear Injector; 2.4.5 Coaxial Centrifugal Injectors; 2.5 Numerical Simulation of Liquid Propellant Atomization; 2.5.1 Theoretical Models of Liquid Propellant Atomization; 2.5.2 Quasi-fluid Models 327 $a2.5.3 Particle Trajectory Models2.5.4 Simulation of Liquid Jet Atomization Using Interface Tracking Method; 2.5.5 Liquid Jet Structure - Varying Flow Conditions; References; Chapter 3 Modeling of Droplet Evaporation and Combustion ; 3.1 Theory for Quasi-Steady Evaporation and Combustion of a Single Droplet at Atmospheric Pressure; 3.1.1 Quasi-Steady Evaporation Theory for Single Droplet in the Static Gas without Combustion; 3.1.2 Quasi-Steady Evaporation Theory for Droplet in a Static Gas with Combustion; 3.1.3 Non-Combustion Evaporation Theory for a Droplet in a Convective Flow 327 $a3.1.4 Evaporation Theory for a Droplet in a Convective Medium with Combustion3.2 Evaporation Model for a Single Droplet under High Pressure; 3.2.1 ZKS Droplet High Pressure Evaporation Theory; 3.2.2 Application of the Liquid Activity Coefficient to Calculate the Gas-Liquid Equilibrium at a High Pressure; 3.3 Subcritical Evaporation Response Characteristics of Propellant Droplet in Oscillatory Environments; 3.3.1 Physical Model; 3.3.2 Examples and the Analysis of Results; 3.4 Multicomponent Fuel Droplet Evaporation Model; 3.4.1 Simple Multicomponent Droplet Evaporation Model 327 $a3.4.2 Continuous Thermodynamics Model of Complex Multicomponent Mixture Droplet Evaporation 606 $aLiquid propellant rockets 606 $aLiquid propellant rocket engines 615 0$aLiquid propellant rockets. 615 0$aLiquid propellant rocket engines. 676 $a629.47522 700 $aWang$b Zhen-Guo$0121343 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910830290403321 996 $aInternal combustion processes of liquid rocket engines$93943441 997 $aUNINA