LEADER 04270nam 2200637 a 450 001 9910968918903321 005 20240416072837.0 010 $a1-60086-050-8 010 $a1-60119-209-6 035 $a(CKB)1000000000327160 035 $a(CtWfDGI)bke00015597 035 $a(SSID)ssj0000071807 035 $a(PQKBManifestationID)11997417 035 $a(PQKBTitleCode)TC0000071807 035 $a(PQKBWorkID)10090640 035 $a(PQKB)11342612 035 $a(MiAaPQ)EBC3111475 035 $a(Au-PeEL)EBL3111475 035 $a(CaPaEBR)ebr10516507 035 $a(OCoLC)922978643 035 $a(BIP)13641474 035 $a(EXLCZ)991000000000327160 100 $a20060524d2006 uy 0 101 0 $aeng 135 $aurzn|||||| 181 $ctxt 182 $cc 183 $acr 200 10$aElements of propulsion $egas turbines and rockets /$fJack D. Mattingly ; foreword by Hans von Ohain 205 $a1st ed. 210 $aReston, Va. $cAmerican Institute of Aeronautics and Astronautics$dc2006 215 $alx, 867 p. $cill 225 1 $aAIAA education series 300 $aTitle from title screen. 311 08$a1-56347-779-3 320 $aIncludes bibliographical references (p. 845-849) and index. 327 $aCover -- Title -- Copyright -- Foreword to the Second Edition -- Table of Contents -- Foreword to the First Edition -- Preface -- Acknowledgments -- Nomenclature -- Chapter 1. Introduction -- Chapter 2. Review of Fundamentals -- Chapter 3. Rocket Propulsion -- Chapter 4. Aircraft Gas Turbine Engine -- Chapter 5. Parametric Cycle Analysis of Ideal Engines -- Chapter 6. Component Performance -- Chapter 7. Parametric Cycle Analysis of Real Engines -- Chapter 8. Engine Performance Analysis -- Chapter 9. Turbomachinery -- Chapter 10. Inlets, Nozzles, and Combustion Systems -- Appendix A. Altitude Tables -- Appendix B. Gas Turbine Engine Data -- Appendix C. Data for Some Liquid-Propellant Rocket Engines -- Appendix D. Air and (CH2)n Properties at Low Pressure -- Appendix E. Turbomachinery Stresses and Materials -- Appendix F. About the Software -- Appendix G. Answers to Selected Problems -- References -- Index -- Supporting Materials -- Back Cover. 330 $aThis text provides a complete introduction to gas turbine and rocket propulsion for aerospace and mechanical engineers. Building on the very successful Elements of Gas Turbine Propulsion, textbook coverage has been expanded to include rocket propulsion and the material on gas dynamics has been dramatically improved. The text is divided into four parts: basic concepts and gas dynamics: analysis of rocket propulsion systems; parametric (design point) and performance (off-design) analysis of air breathing propulsion systems; and analysis and design of major gas turbine engine components (fans, compressors, turbines, inlets, nozzles, main burners, and afterburners). Design concepts are introduced early (aircraft and rocket performance in an introductory chapter) and integrated throughout. Written with extensive student input on the design of the book, the book builds upon definitions and gradually develops the thermodynamics, gas dynamics, rocket engine analysis, and gas turbine engine principles. The book contains over 100 worked examples and numerous homework problems so concepts are applied after they are introduced. Over 600 illustrations and pictures show basic concepts, trends, and design examples. Eight computer programs accompany the text, which allow for rapid calculation of trends, "what if" questions, conceptual design, homework problems, and homework verification. The software runs in the Windows operating system on PC-compatible systems. 410 0$aAIAA education series. 606 $aAircraft gas-turbines 606 $aAirplanes$xJet propulsion 606 $aJet engines 606 $aRocket engines 615 0$aAircraft gas-turbines. 615 0$aAirplanes$xJet propulsion. 615 0$aJet engines. 615 0$aRocket engines. 676 $a629.134/353 700 $aMattingly$b Jack D$0314162 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910968918903321 996 $aElements of propulsion$91226174 997 $aUNINA