Theory of aerospace propulsion:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Amsterdam [u.a.]
Elsevier, Butterworth-Heinemann
2012
|
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Beschreibung: | Readers of this book will be able to: utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems and be able to determine the applicability of each, perform system studies of aircraft engine systems for specified flight conditions, perform preliminary aerothermal design of turbomachinery components, and conceive, analyze, and optimize competing preliminary designs for conventional and unconventional missions. Early coverage of cycle analysis provides a systems perspective, and offers context for the chapters on turbomachinery and components Broader coverage than found in most other books - including coverage of propellers, nuclear rockets, and space propulsion - allows analysis and design of more types of propulsion systems In depth, quantitative treatments of the components of jet propulsion engines provides the tools for evaluation and component matching for optimal system performance Worked examples and end of chapter exercises provide practice for analysis, preliminary design, and systems integration Chapter 1 IDEALIZED FLOW MACHINES -- Chapter 2 QUASI-ONE-DIMENSIONAL FLOW EQUATIONS -- Chapter 3 IDEALIZED CYCLE ANALYSIS OF JET ENGINES -- Chapter 4 COMBUSTION CHAMBERS FOR AIRBREATHING ENGINES -- Chapter 5 NOZZLES -- Chapter 6 INLETS -- Chapter 7 TURBOMACHINERY -- Chapter 8 BLADE ELEMENT ANALYSIS OF AXIAL FLOW TURBOMACHINES -- Chapter 9. TURBINE ENGINE PERFORMANCE AND COMPONENT INTEGRATION -- Chapter 10 PROPELLERS -- Chapter 11 LIQUID ROCKETS -- Chapter 12 SOLID PROPELLANT ROCKETS -- Chapter 13 NUCLEAR ROCKETS -- Chapter 14 SPACE PROPULSION -- Chapter 15. PROPULSION ASPECTS OF HIGH-SPEED FLIGHT -- Appendix A: SHOCK WAVES, EXPANSIONS, TABLES AND CHARTS -- Appendix B: PROPERTIES OF HYDROCARBON FUEL COMBUSTION -- Appendix C: EARTH'S ATMOSPHERE -- Appendix D: BOOST PHASE AND STAGING OF ROCKETS -- Appendix E: SAFETY, RELIABILITY, AND RISK ASSESSMENT -- Appendix F: AIRCRAFT PERFORMANCE -- Appendix G: THERMODYNAMIC PROPERTIES OF SELECTED SPECIES. Includes bibliographical references and index |
| Beschreibung: | 1 Online-Ressource (p) cm |
| ISBN: | 9781856179126 1856179125 |
Internformat
MARC
| LEADER | 00000nmm a2200000zc 4500 | ||
|---|---|---|---|
| 001 | BV039829626 | ||
| 003 | DE-604 | ||
| 005 | 20161010 | ||
| 007 | cr|uuu---uuuuu | ||
| 008 | 120124s2012 sz |||| o||u| ||||||eng d | ||
| 020 | |a 9781856179126 |c Online |9 978-1-85617-912-6 | ||
| 020 | |a 9781856179126 |c Print |9 978-1-85617-912-6 | ||
| 020 | |a 1856179125 |c electronic bk. |9 1-85617-912-5 | ||
| 024 | 7 | |a 10.1016/B978-1-85617-912-6.01001-X |2 doi | |
| 035 | |a (OCoLC)760173083 | ||
| 035 | |a (DE-599)BVBBV039829626 | ||
| 040 | |a DE-604 |b ger |e aacr | ||
| 041 | 0 | |a eng | |
| 044 | |a sz |c XA-CH | ||
| 049 | |a DE-1046 |a DE-1028 |a DE-83 |a DE-706 | ||
| 082 | 0 | |a 629.1/1 |2 23 | |
| 084 | |a VER 630f |2 stub | ||
| 084 | |a VER 720f |2 stub | ||
| 100 | 1 | |a Sforza, P. M. |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Theory of aerospace propulsion |c Pasquale M. Sforza |
| 264 | 1 | |a Amsterdam [u.a.] |b Elsevier, Butterworth-Heinemann |c 2012 | |
| 300 | |a 1 Online-Ressource (p) |c cm | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b c |2 rdamedia | ||
| 338 | |b cr |2 rdacarrier | ||
| 500 | |a Readers of this book will be able to: utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems and be able to determine the applicability of each, perform system studies of aircraft engine systems for specified flight conditions, perform preliminary aerothermal design of turbomachinery components, and conceive, analyze, and optimize competing preliminary designs for conventional and unconventional missions. Early coverage of cycle analysis provides a systems perspective, and offers context for the chapters on turbomachinery and components Broader coverage than found in most other books - including coverage of propellers, nuclear rockets, and space propulsion - allows analysis and design of more types of propulsion systems In depth, quantitative treatments of the components of jet propulsion engines provides the tools for evaluation and component matching for optimal system performance Worked examples and end of chapter exercises provide practice for analysis, preliminary design, and systems integration | ||
| 500 | |a Chapter 1 IDEALIZED FLOW MACHINES -- Chapter 2 QUASI-ONE-DIMENSIONAL FLOW EQUATIONS -- Chapter 3 IDEALIZED CYCLE ANALYSIS OF JET ENGINES -- Chapter 4 COMBUSTION CHAMBERS FOR AIRBREATHING ENGINES -- Chapter 5 NOZZLES -- Chapter 6 INLETS -- Chapter 7 TURBOMACHINERY -- Chapter 8 BLADE ELEMENT ANALYSIS OF AXIAL FLOW TURBOMACHINES -- Chapter 9. TURBINE ENGINE PERFORMANCE AND COMPONENT INTEGRATION -- Chapter 10 PROPELLERS -- Chapter 11 LIQUID ROCKETS -- Chapter 12 SOLID PROPELLANT ROCKETS -- Chapter 13 NUCLEAR ROCKETS -- Chapter 14 SPACE PROPULSION -- Chapter 15. PROPULSION ASPECTS OF HIGH-SPEED FLIGHT -- Appendix A: SHOCK WAVES, EXPANSIONS, TABLES AND CHARTS -- Appendix B: PROPERTIES OF HYDROCARBON FUEL COMBUSTION -- Appendix C: EARTH'S ATMOSPHERE -- Appendix D: BOOST PHASE AND STAGING OF ROCKETS -- Appendix E: SAFETY, RELIABILITY, AND RISK ASSESSMENT -- Appendix F: AIRCRAFT PERFORMANCE -- Appendix G: THERMODYNAMIC PROPERTIES OF SELECTED SPECIES. | ||
| 500 | |a Includes bibliographical references and index | ||
| 650 | 4 | |a Jet propulsion | |
| 650 | 0 | 7 | |a Flugtriebwerk |0 (DE-588)4154773-1 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Raketentriebwerk |0 (DE-588)4176905-3 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Luftstrahltriebwerk |0 (DE-588)4128278-4 |2 gnd |9 rswk-swf |
| 689 | 0 | 0 | |a Flugtriebwerk |0 (DE-588)4154773-1 |D s |
| 689 | 0 | |5 DE-604 | |
| 689 | 1 | 0 | |a Raketentriebwerk |0 (DE-588)4176905-3 |D s |
| 689 | 1 | |5 DE-604 | |
| 689 | 2 | 0 | |a Luftstrahltriebwerk |0 (DE-588)4128278-4 |D s |
| 689 | 2 | |8 1\p |5 DE-604 | |
| 710 | 2 | |a ScienceDirect (Online service) |e Sonstige |4 oth | |
| 856 | 4 | 0 | |u http://www.sciencedirect.com/science/book/9781856179126 |x Verlag |3 Volltext |
| 912 | |a ZDB-33-EGE |a ZDB-33-ESD |a ebook |a ZDB-33-EBS | ||
| 940 | 1 | |q FAW_PDA_ESD | |
| 940 | 1 | |q TUM_PDA_ELSEVIER_erworben | |
| 940 | 1 | |q UBY_PDA_ESDENG_Kauf | |
| 940 | 1 | |q FLA_PDA_ESD | |
| 999 | |a oai:aleph.bib-bvb.de:BVB01-024689630 | ||
| 883 | 1 | |8 1\p |a cgwrk |d 20201028 |q DE-101 |u https://d-nb.info/provenance/plan#cgwrk | |
Datensatz im Suchindex
| _version_ | 1804148764501344256 |
|---|---|
| any_adam_object | |
| author | Sforza, P. M. |
| author_facet | Sforza, P. M. |
| author_role | aut |
| author_sort | Sforza, P. M. |
| author_variant | p m s pm pms |
| building | Verbundindex |
| bvnumber | BV039829626 |
| classification_tum | VER 630f VER 720f |
| collection | ZDB-33-EGE ZDB-33-ESD ebook ZDB-33-EBS |
| ctrlnum | (OCoLC)760173083 (DE-599)BVBBV039829626 |
| dewey-full | 629.1/1 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.1/1 |
| dewey-search | 629.1/1 |
| dewey-sort | 3629.1 11 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Verkehrstechnik Verkehr / Transport |
| format | Electronic eBook |
| fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>04143nmm a2200589zc 4500</leader><controlfield tag="001">BV039829626</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">20161010 </controlfield><controlfield tag="007">cr|uuu---uuuuu</controlfield><controlfield tag="008">120124s2012 sz |||| o||u| ||||||eng d</controlfield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">9781856179126</subfield><subfield code="c">Online</subfield><subfield code="9">978-1-85617-912-6</subfield></datafield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">9781856179126</subfield><subfield code="c">Print</subfield><subfield code="9">978-1-85617-912-6</subfield></datafield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">1856179125</subfield><subfield code="c">electronic bk.</subfield><subfield code="9">1-85617-912-5</subfield></datafield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1016/B978-1-85617-912-6.01001-X</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(OCoLC)760173083</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV039829626</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-604</subfield><subfield code="b">ger</subfield><subfield code="e">aacr</subfield></datafield><datafield tag="041" ind1="0" ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="044" ind1=" " ind2=" "><subfield code="a">sz</subfield><subfield code="c">XA-CH</subfield></datafield><datafield tag="049" ind1=" " ind2=" "><subfield code="a">DE-1046</subfield><subfield code="a">DE-1028</subfield><subfield code="a">DE-83</subfield><subfield code="a">DE-706</subfield></datafield><datafield tag="082" ind1="0" ind2=" "><subfield code="a">629.1/1</subfield><subfield code="2">23</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">VER 630f</subfield><subfield code="2">stub</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">VER 720f</subfield><subfield code="2">stub</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Sforza, P. M.</subfield><subfield code="e">Verfasser</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Theory of aerospace propulsion</subfield><subfield code="c">Pasquale M. Sforza</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Amsterdam [u.a.]</subfield><subfield code="b">Elsevier, Butterworth-Heinemann</subfield><subfield code="c">2012</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">1 Online-Ressource (p)</subfield><subfield code="c">cm</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">Readers of this book will be able to: utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems and be able to determine the applicability of each, perform system studies of aircraft engine systems for specified flight conditions, perform preliminary aerothermal design of turbomachinery components, and conceive, analyze, and optimize competing preliminary designs for conventional and unconventional missions. Early coverage of cycle analysis provides a systems perspective, and offers context for the chapters on turbomachinery and components Broader coverage than found in most other books - including coverage of propellers, nuclear rockets, and space propulsion - allows analysis and design of more types of propulsion systems In depth, quantitative treatments of the components of jet propulsion engines provides the tools for evaluation and component matching for optimal system performance Worked examples and end of chapter exercises provide practice for analysis, preliminary design, and systems integration</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">Chapter 1 IDEALIZED FLOW MACHINES -- Chapter 2 QUASI-ONE-DIMENSIONAL FLOW EQUATIONS -- Chapter 3 IDEALIZED CYCLE ANALYSIS OF JET ENGINES -- Chapter 4 COMBUSTION CHAMBERS FOR AIRBREATHING ENGINES -- Chapter 5 NOZZLES -- Chapter 6 INLETS -- Chapter 7 TURBOMACHINERY -- Chapter 8 BLADE ELEMENT ANALYSIS OF AXIAL FLOW TURBOMACHINES -- Chapter 9. TURBINE ENGINE PERFORMANCE AND COMPONENT INTEGRATION -- Chapter 10 PROPELLERS -- Chapter 11 LIQUID ROCKETS -- Chapter 12 SOLID PROPELLANT ROCKETS -- Chapter 13 NUCLEAR ROCKETS -- Chapter 14 SPACE PROPULSION -- Chapter 15. PROPULSION ASPECTS OF HIGH-SPEED FLIGHT -- Appendix A: SHOCK WAVES, EXPANSIONS, TABLES AND CHARTS -- Appendix B: PROPERTIES OF HYDROCARBON FUEL COMBUSTION -- Appendix C: EARTH'S ATMOSPHERE -- Appendix D: BOOST PHASE AND STAGING OF ROCKETS -- Appendix E: SAFETY, RELIABILITY, AND RISK ASSESSMENT -- Appendix F: AIRCRAFT PERFORMANCE -- Appendix G: THERMODYNAMIC PROPERTIES OF SELECTED SPECIES.</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">Includes bibliographical references and index</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Jet propulsion</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Flugtriebwerk</subfield><subfield code="0">(DE-588)4154773-1</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Raketentriebwerk</subfield><subfield code="0">(DE-588)4176905-3</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Luftstrahltriebwerk</subfield><subfield code="0">(DE-588)4128278-4</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="689" ind1="0" ind2="0"><subfield code="a">Flugtriebwerk</subfield><subfield code="0">(DE-588)4154773-1</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2=" "><subfield code="5">DE-604</subfield></datafield><datafield tag="689" ind1="1" ind2="0"><subfield code="a">Raketentriebwerk</subfield><subfield code="0">(DE-588)4176905-3</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="1" ind2=" "><subfield code="5">DE-604</subfield></datafield><datafield tag="689" ind1="2" ind2="0"><subfield code="a">Luftstrahltriebwerk</subfield><subfield code="0">(DE-588)4128278-4</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="2" ind2=" "><subfield code="8">1\p</subfield><subfield code="5">DE-604</subfield></datafield><datafield tag="710" ind1="2" ind2=" "><subfield code="a">ScienceDirect (Online service)</subfield><subfield code="e">Sonstige</subfield><subfield code="4">oth</subfield></datafield><datafield tag="856" ind1="4" ind2="0"><subfield code="u">http://www.sciencedirect.com/science/book/9781856179126</subfield><subfield code="x">Verlag</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">ZDB-33-EGE</subfield><subfield code="a">ZDB-33-ESD</subfield><subfield code="a">ebook</subfield><subfield code="a">ZDB-33-EBS</subfield></datafield><datafield tag="940" ind1="1" ind2=" "><subfield code="q">FAW_PDA_ESD</subfield></datafield><datafield tag="940" ind1="1" ind2=" "><subfield code="q">TUM_PDA_ELSEVIER_erworben</subfield></datafield><datafield tag="940" ind1="1" ind2=" "><subfield code="q">UBY_PDA_ESDENG_Kauf</subfield></datafield><datafield tag="940" ind1="1" ind2=" "><subfield code="q">FLA_PDA_ESD</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-024689630</subfield></datafield><datafield tag="883" ind1="1" ind2=" "><subfield code="8">1\p</subfield><subfield code="a">cgwrk</subfield><subfield code="d">20201028</subfield><subfield code="q">DE-101</subfield><subfield code="u">https://d-nb.info/provenance/plan#cgwrk</subfield></datafield></record></collection> |
| id | DE-604.BV039829626 |
| illustrated | Not Illustrated |
| indexdate | 2024-07-10T00:12:19Z |
| institution | BVB |
| isbn | 9781856179126 1856179125 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-024689630 |
| oclc_num | 760173083 |
| open_access_boolean | |
| owner | DE-1046 DE-1028 DE-83 DE-706 |
| owner_facet | DE-1046 DE-1028 DE-83 DE-706 |
| physical | 1 Online-Ressource (p) cm |
| psigel | ZDB-33-EGE ZDB-33-ESD ebook ZDB-33-EBS FAW_PDA_ESD TUM_PDA_ELSEVIER_erworben UBY_PDA_ESDENG_Kauf FLA_PDA_ESD |
| publishDate | 2012 |
| publishDateSearch | 2012 |
| publishDateSort | 2012 |
| publisher | Elsevier, Butterworth-Heinemann |
| record_format | marc |
| spelling | Sforza, P. M. Verfasser aut Theory of aerospace propulsion Pasquale M. Sforza Amsterdam [u.a.] Elsevier, Butterworth-Heinemann 2012 1 Online-Ressource (p) cm txt rdacontent c rdamedia cr rdacarrier Readers of this book will be able to: utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems and be able to determine the applicability of each, perform system studies of aircraft engine systems for specified flight conditions, perform preliminary aerothermal design of turbomachinery components, and conceive, analyze, and optimize competing preliminary designs for conventional and unconventional missions. Early coverage of cycle analysis provides a systems perspective, and offers context for the chapters on turbomachinery and components Broader coverage than found in most other books - including coverage of propellers, nuclear rockets, and space propulsion - allows analysis and design of more types of propulsion systems In depth, quantitative treatments of the components of jet propulsion engines provides the tools for evaluation and component matching for optimal system performance Worked examples and end of chapter exercises provide practice for analysis, preliminary design, and systems integration Chapter 1 IDEALIZED FLOW MACHINES -- Chapter 2 QUASI-ONE-DIMENSIONAL FLOW EQUATIONS -- Chapter 3 IDEALIZED CYCLE ANALYSIS OF JET ENGINES -- Chapter 4 COMBUSTION CHAMBERS FOR AIRBREATHING ENGINES -- Chapter 5 NOZZLES -- Chapter 6 INLETS -- Chapter 7 TURBOMACHINERY -- Chapter 8 BLADE ELEMENT ANALYSIS OF AXIAL FLOW TURBOMACHINES -- Chapter 9. TURBINE ENGINE PERFORMANCE AND COMPONENT INTEGRATION -- Chapter 10 PROPELLERS -- Chapter 11 LIQUID ROCKETS -- Chapter 12 SOLID PROPELLANT ROCKETS -- Chapter 13 NUCLEAR ROCKETS -- Chapter 14 SPACE PROPULSION -- Chapter 15. PROPULSION ASPECTS OF HIGH-SPEED FLIGHT -- Appendix A: SHOCK WAVES, EXPANSIONS, TABLES AND CHARTS -- Appendix B: PROPERTIES OF HYDROCARBON FUEL COMBUSTION -- Appendix C: EARTH'S ATMOSPHERE -- Appendix D: BOOST PHASE AND STAGING OF ROCKETS -- Appendix E: SAFETY, RELIABILITY, AND RISK ASSESSMENT -- Appendix F: AIRCRAFT PERFORMANCE -- Appendix G: THERMODYNAMIC PROPERTIES OF SELECTED SPECIES. Includes bibliographical references and index Jet propulsion Flugtriebwerk (DE-588)4154773-1 gnd rswk-swf Raketentriebwerk (DE-588)4176905-3 gnd rswk-swf Luftstrahltriebwerk (DE-588)4128278-4 gnd rswk-swf Flugtriebwerk (DE-588)4154773-1 s DE-604 Raketentriebwerk (DE-588)4176905-3 s Luftstrahltriebwerk (DE-588)4128278-4 s 1\p DE-604 ScienceDirect (Online service) Sonstige oth http://www.sciencedirect.com/science/book/9781856179126 Verlag Volltext 1\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk |
| spellingShingle | Sforza, P. M. Theory of aerospace propulsion Jet propulsion Flugtriebwerk (DE-588)4154773-1 gnd Raketentriebwerk (DE-588)4176905-3 gnd Luftstrahltriebwerk (DE-588)4128278-4 gnd |
| subject_GND | (DE-588)4154773-1 (DE-588)4176905-3 (DE-588)4128278-4 |
| title | Theory of aerospace propulsion |
| title_auth | Theory of aerospace propulsion |
| title_exact_search | Theory of aerospace propulsion |
| title_full | Theory of aerospace propulsion Pasquale M. Sforza |
| title_fullStr | Theory of aerospace propulsion Pasquale M. Sforza |
| title_full_unstemmed | Theory of aerospace propulsion Pasquale M. Sforza |
| title_short | Theory of aerospace propulsion |
| title_sort | theory of aerospace propulsion |
| topic | Jet propulsion Flugtriebwerk (DE-588)4154773-1 gnd Raketentriebwerk (DE-588)4176905-3 gnd Luftstrahltriebwerk (DE-588)4128278-4 gnd |
| topic_facet | Jet propulsion Flugtriebwerk Raketentriebwerk Luftstrahltriebwerk |
| url | http://www.sciencedirect.com/science/book/9781856179126 |
| work_keys_str_mv | AT sforzapm theoryofaerospacepropulsion AT sciencedirectonlineservice theoryofaerospacepropulsion |