Theory of aerospace propulsion

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 syst...

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Bibliographic Details
Main Author: Sforza, P. M.
Format: eBook
Language: English
Published: Waltham, MA : Academic Press, ©2012.
Subjects:
ISBN: 9781856179126
1856179125
9780123848895
012384889X
Physical Description: 1 online resource

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Table of contents

LEADER 03884cam a2200373 a 4500
001 kn-ocn760173083
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 111110s2012 mau ob 001 0 eng d
040 |a OPELS  |b eng  |e pn  |c OPELS  |d CDX  |d OCLCO  |d OCLCQ  |d E7B  |d TEF  |d N$T  |d YDXCP  |d OCLCQ  |d DEBSZ  |d OCLCQ  |d ZCU  |d OCLCQ  |d OCLCF  |d UIU  |d OCLCQ  |d STF  |d OCLCQ  |d DKU  |d U3W  |d CNNOR  |d LOA  |d CEF  |d RRP  |d OCLCQ  |d WYU  |d LVT  |d TKN  |d LEAUB  |d OL$  |d OCLCQ  |d OCLCO  |d S2H  |d OCLCO  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB 
020 |a 9781856179126  |q (electronic bk.) 
020 |a 1856179125  |q (electronic bk.) 
020 |a 9780123848895  |q (electronic bk.) 
020 |a 012384889X  |q (electronic bk.) 
035 |a (OCoLC)760173083  |z (OCoLC)769188143  |z (OCoLC)775115980  |z (OCoLC)969545984 
100 1 |a Sforza, P. M. 
245 1 0 |a Theory of aerospace propulsion /  |c Pasquale M. Sforza. 
260 |a Waltham, MA :  |b Academic Press,  |c ©2012. 
300 |a 1 online resource 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
520 |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. 
505 0 |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. 
504 |a Includes bibliographical references and index. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Jet propulsion. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
776 0 8 |i Print version:  |a Sforza, P.M.  |t Theory of aerospace propulsion.  |d Waltham, MA : Academic Press, ©2012  |z 9781856179126  |w (DLC) 2011027614  |w (OCoLC)714729590 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpTAP00004/theory-of-aerospace?kpromoter=marc  |y Full text