LEADER 01189nam0-22003971i-450- 001 990007953840403321 005 20091116164205.0 010 $a88-343-1058-6 035 $a000795384 035 $aFED01000795384 035 $a(Aleph)000795384FED01 035 $a000795384 100 $a20041119d2003----km-y0itay50------ba 101 1 $aita$ceng 102 $aIT 105 $a--------001cy 200 1 $a<>nuova condizione umana$fZygmunt Bauman$gpresentazione di Mauro Magatti$gtraduzioni di Maura Micheloni e Elena Midolo 210 $aMilano$cVita & pensiero$dc2003 215 $a155 p.$d21 cm 225 1 $aTransizioni$v13 610 0 $aGlobalizzazione$aAspetti sociali 610 0 $aCambiamento sociale$aEconomia$aAspetti sociali 676 $a301.01$v22$zita 676 $a303.4$v22$zita 676 $a306.3$v22$zita 700 1$aBauman,$bZygmunt$f<1925- >$0124491 702 1$aMagatti,$bMauro 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990007953840403321 952 $a14340 BAU/03$b20554$fSES 952 $a301.01 BAU 16$b4742$fBFS 959 $aSES 959 $aBFS 996 $aNuova condizione umana$9252578 997 $aUNINA LEADER 01876nam 2200493 450 001 9910702698303321 005 20140911163806.0 035 $a(CKB)5470000002429201 035 $a(OCoLC)890410905 035 $a(EXLCZ)995470000002429201 100 $a20140911j19830906 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aPerformance analysis of a concatenated coding scheme for error control /$fDaniel J. Costello, Jr., Shu Lin 210 1$aChicago, Illinois :$cDepartment of Electrical Engineering, Illinois Institute of Technology ;$aGreenbelt, Maryland :$cGoddard Space Flight Center,$dSeptember 6, 1983. 215 $a1 online resource (12 pages, 2 unnumbered pages) $cillustrations 225 1 $aNASA-CR ;$v175345 300 $aTitle from title screen (viewed on Sept. 11, 2014). 300 $a"September 6, 1983." 320 $aIncludes bibliographical references (page 10). 606 $aConcatenated codes$2nasat 606 $aError correcting codes$2nasat 606 $aError detection codes$2nasat 606 $aPolynomials$2nasat 606 $aSpace exploration$2nasat 615 7$aConcatenated codes. 615 7$aError correcting codes. 615 7$aError detection codes. 615 7$aPolynomials. 615 7$aSpace exploration. 700 $aCostello$b Daniel J.$f1942-$044016 702 $aLin$b Shu$f1937- 712 02$aIllinois Institute of Technology.$bDepartment of Electrical Engineering, 712 02$aGoddard Space Flight Center. 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910702698303321 996 $aPerformance analysis of a concatenated coding scheme for error control$93451087 997 $aUNINA LEADER 05542nam 2200733Ia 450 001 9910810633003321 005 20240514064230.0 010 $a1-280-59273-7 010 $a9786613622563 010 $a1-118-13068-5 010 $a1-118-12757-9 035 $a(CKB)2670000000177259 035 $a(EBL)817344 035 $a(OCoLC)773534870 035 $a(SSID)ssj0000632079 035 $a(PQKBManifestationID)11386429 035 $a(PQKBTitleCode)TC0000632079 035 $a(PQKBWorkID)10599640 035 $a(PQKB)11560265 035 $a(MiAaPQ)EBC817344 035 $a(Au-PeEL)EBL817344 035 $a(CaPaEBR)ebr10560537 035 $a(CaONFJC)MIL362256 035 $a(PPN)190591862 035 $a(EXLCZ)992670000000177259 100 $a20120112d2012 uy 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt 182 $cc 183 $acr 200 10$aApplications of turbulent and multiphase combustion /$fKenneth K. Kuo, Ragini Acharya 205 $a1st ed. 210 $aHoboken, N.J. $cWiley$dc2012 215 $a1 online resource (602 p.) 300 $aDescription based upon print version of record. 311 $a1-118-12756-0 320 $aIncludes bibliographical references and index. 327 $aApplications of Turbulent and Multiphase Combustion; Contents; Preface; Chapter 1 Solid Propellants and Their Combustion Characteristics; 1.1 Background of Solid Propellant Combustion; 1.1.1 Definition of Solid Propellants; 1.1.2 Desirable Characteristics of Solid Propellants; 1.1.3 Calculation of Oxygen Balance; 1.1.4 Homogeneous Propellants; 1.1.4.1 Decomposition Characteristics of NC; 1.1.5 Heterogeneous Propellants (or Composite Propellants); 1.1.6 Major Types of Ingredients in Solid Propellants; 1.1.6.1 Description of Oxidizer Ingredients; 1.1.6.2 Description of Fuel Binders 327 $a1.1.6.3 Curing and Cross-Linking Agents 1.1.6.4 Aging; 1.1.7 Applications of Solid Propellants; 1.1.7.1 Hazard Classifications of Solid Propellants; 1.1.8 Material Characterization of Propellants; 1.1.8.1 Propellant Density Calculation; 1.1.8.2 Propellant Mass Fraction,; 1.1.8.3 Viscoelastic Behavior of Solid Propellants; 1.1.9 Thermal Profile in a Burning Solid Propellant; 1.1.9.1 Surface and Subsurface Temperature Measurements of Solid Propellants; 1.1.9.2 Interfacial Energy Flux Balance at the Solid Propellant Surface; 1.1.9.3 Energy Equation for the Gas Phase 327 $a1.1.9.4 Burning Rate of Solid Propellants 1.1.9.5 Temperature Sensitivity of Burning Rate; 1.1.9.6 Measurement of Propellant Burning Rate by Using a Strand Burner; 1.1.9.7 Measurement of Propellant Burning Rate by Using a Small-Scale Motor; 1.1.9.8 Burning Rate Temperature Sensitivity of Neat Ingredients; 1.2 Solid-Propellant Rocket and Gun Performance Parameters; 1.2.1 Performance Parameters of a Solid Rocket Motor; 1.2.1.1 Thrust of a Solid Rocket Motor; 1.2.1.2 Specific Impulse of a Solid Rocket Motor; 1.2.1.3 Density-Specific Impulse; 1.2.1.4 Effective Vacuum Exhaust Velocity 327 $a1.2.1.5 Characteristic Velocity C*1.2.1.6 Pressure Sensitivity of Burning Rate; 1.2.1.7 Thrust Coefficient Efficiency; 1.2.1.8 Effect of Pressure Exponent on Stable/Unstable Burning in Solid Rocket Motor; 1.2.2 Performance Parameters of Solid-Propellant Gun Systems; 1.2.2.1 Energy Balance Equation; 1.2.2.2 Efficiencies of Gun Propulsion Systems; 1.2.2.3 Heat of Explosion (Hoex); 1.2.2.4 Relative Quickness, Relative Force, and Deviations in Muzzle Velocity; 1.2.2.5 Dynamic Vivacity; Chapter 2 Thermal Decomposition and Combustion of Nitramines 327 $a2.1 Thermophysical Properties of Selected Nitramines 2.2 Polymorphic Forms of Nitramines; 2.2.1 Polymorphic Forms of HMX; 2.2.2 Polymorphic Forms of RDX; 2.3 Thermal Decomposition of RDX; 2.3.1 Explanation of Opposite Trends on ?- and ?-RDX Decomposition with Increasing Pressure; 2.3.2 Thermal Decomposition Mechanisms of RDX; 2.3.2.1 Homolytic N-N Bond Cleavage; 2.3.2.2 Concerted Ring Opening Mechanism of RDX; 2.3.2.3 Successive HONO Elimination Mechanism of RDX; 2.3.2.4 Analysis of Three Decomposition Mechanisms; 2.3.3 Formation of Foam Layer Near RDX Burning Surface 327 $a2.4 Gas-Phase Reactions of RDX 330 $aA hands-on, integrated approach to solving combustion problems in diverse areas An understanding of turbulence, combustion, and multiphase reacting flows is essential for engineers and scientists in many industries, including power generation, jet and rocket propulsion, pollution control, fire prevention and safety, and material processing. This book offers a highly practical discussion of burning behavior and chemical processes occurring in diverse materials, arming readers with the tools they need to solve the most complex combustion problems facing the scientific community today. 606 $aCombustion engineering 606 $aTurbulence 606 $aMultiphase flow$xMathematical models 606 $aCombustion$xMathematical models 615 0$aCombustion engineering. 615 0$aTurbulence. 615 0$aMultiphase flow$xMathematical models. 615 0$aCombustion$xMathematical models. 676 $a621.402/3 686 $aSCI065000$2bisacsh 700 $aKuo$b Kenneth K$013378 701 $aAcharya$b Ragini$01646622 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910810633003321 996 $aApplications of turbulent and multiphase combustion$94077240 997 $aUNINA