LEADER 03645nam 2200673Ia 450 001 9910954236303321 005 20251117083841.0 010 $a1-60086-840-1 010 $a1-60086-841-X 035 $a(CKB)2670000000187715 035 $a(EBL)3111689 035 $a(SSID)ssj0000830904 035 $a(PQKBManifestationID)11530810 035 $a(PQKBTitleCode)TC0000830904 035 $a(PQKBWorkID)10838908 035 $a(PQKB)10502474 035 $a(Au-PeEL)EBL3111689 035 $a(CaPaEBR)ebr10525584 035 $a(OCoLC)802058718 035 $a(MiAaPQ)EBC3111689 035 $a(BIP)37308797 035 $a(EXLCZ)992670000000187715 100 $a20111018d2011 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 00$aExergy analysis and design optimization for aerospace vehicles and systems /$fedited by Jose A. Camberos, David J. Moorhouse 205 $a1st ed. 210 $aReston, VA $cAmerican Institute of Aeronautics and Astronautics$dc2011 215 $a1 online resource (658 p.) 225 1 $aProgress in astronautics and aeronautics ;$vv. 238 300 $aDescription based upon print version of record. 311 08$a1-60086-839-8 320 $aIncludes bibliographical references and index. 327 $a""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Contents""; ""Preface""; ""Acknowledgments""; ""Nomenclature""; ""Chapter 1 Introduction""; ""Chapter 2 Fundamentals of Exergy Analysis""; ""Chapter 3 Applications of Exergy Analysis""; ""Chapter 4 Integrated Subsystem Analysis Using EntropyGeneration Minimization""; ""Chapter 5 Exergy-Based Design Methodology for Airfoil ShapeOptimization and Wing Analysis""; ""Chapter 6 Entropy Generation and Aerospace VehiclePerformance""; ""Chapter 7 Optimization Using Entropy-GenerationMinimization for Maximum Performance of Hypersonic Vehicles"" 327 $a""Chapter 8 Characterization of Aerospace Vehicle Performanceand Mission Analysis Using Exergy""""Chapter 9 Mission-Integrated Synthesis and DesignOptimization (MIS/DO) of Aerospace Vehicles""; ""Chapter 10 MIS/DO Applied to High Performance AerospaceVehicles""; ""Chapter 11 Thermodynamics, Entropy GenerationMinimization, and the Constructal Law""; ""Chapter 12 Quantum Thermodynamics and the Modeling ofNonequilibrium Phenomena: Theory and Future Directions""; ""Chapter 13 Numerical Methods in Light of the Second Law""; ""Postlude""; ""Index""; ""Supporting Materials"" 330 $aRecognizing a critical need for a holistic approach to systems integration and multidisciplinary analysis and design optimization, the editors pioneered the application of a powerful scientific principle, the second law of thermodynamics, for aerospace engineering. 410 0$aProgress in astronautics and aeronautics ;$vv. 238. 517 3 $aAerospace vehicles and systems 606 $aSpace vehicles$xDesign and construction 606 $aSpace vehicles$xThermodynamics 606 $aAerospace engineering 606 $aExergy 615 0$aSpace vehicles$xDesign and construction. 615 0$aSpace vehicles$xThermodynamics. 615 0$aAerospace engineering. 615 0$aExergy. 701 $aCamberos$b Jose A$0632247 701 $aMoorhouse$b David J$g(David John),$f1939-$01863876 712 02$aAmerican Institute of Aeronautics and Astronautics. 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910954236303321 996 $aExergy analysis and design optimization for aerospace vehicles and systems$94470569 997 $aUNINA