MARC details
| 000 -LEADER |
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| fixed length control field |
03267nam a2200409 a 4500 |
| 001 - CONTROL NUMBER |
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| control field |
BDZ0012905572 |
| 003 - CONTROL NUMBER IDENTIFIER |
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| control field |
StDuBDS |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
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| control field |
20190531161550.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
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| fixed length control field |
110711s2012 ne a f 001 0 eng|d |
| 010 ## - LIBRARY OF CONGRESS CONTROL NUMBER |
|---|
| LC control number |
2011027614 |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
|---|
| International Standard Book Number |
9781856179126: |
| Terms of availability |
£49.99 |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
|---|
| International Standard Book Number |
1856179125 |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
|---|
| International Standard Book Number |
9780123848895 |
| 040 ## - CATALOGING SOURCE |
|---|
| Original cataloging agency |
StDuBDS |
| Transcribing agency |
StDuBDS |
| Modifying agency |
StDuBDSZ |
| 050 #0 - LIBRARY OF CONGRESS CALL NUMBER |
|---|
| Item number |
.S38 2012 |
| 072 #7 - SUBJECT CATEGORY CODE |
|---|
| Subject category code |
TRA |
| Source |
ukslc |
| 072 #7 - SUBJECT CATEGORY CODE |
|---|
| Subject category code |
TRP |
| Source |
thema |
| 082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER |
|---|
| Classification number |
629.11 |
| 100 1# - MAIN ENTRY--PERSONAL NAME |
|---|
| Personal name |
Sforza, P. M. |
| 245 10 - TITLE STATEMENT |
|---|
| Title |
Theory of aerospace propulsion / |
| Statement of responsibility, etc. |
Pasquale M. Sforza. |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. |
|---|
| Place of publication, distribution, etc. |
Amsterdam ; |
| -- |
London : |
| Name of publisher, distributor, etc. |
Butterworth-Heinemann, |
| Date of publication, distribution, etc. |
c2012. |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Extent |
xviii, 684 p. : |
| Other physical details |
ill. ; |
| Dimensions |
25 cm. |
| 504 ## - BIBLIOGRAPHY, ETC. NOTE |
|---|
| Bibliography, etc. note |
Includes bibliographical references and index. |
| 505 0# - FORMATTED CONTENTS NOTE |
|---|
| Formatted contents note |
Idealized flow machines -- quasi-one-dimensional flow equations -- idealized cycle analysis of jet engines -- combustion chambers for airbreathing engines -- nozzles -- inlets -- turbomachinery -- blade element analysis of axial flow turbomachines -- turbine engine performance and component integration -- propellers -- liquid rockets -- solid propellant rockets -- nuclear rockets -- space propulsion -- 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. |
| 520 ## - SUMMARY, ETC. |
|---|
| Summary, etc. |
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. |
| 590 ## - LOCAL NOTE (RLIN) |
|---|
| a |
56.23 |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Jet propulsion. |
| 650 #7 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Transport. |
| Source of heading or term |
ukslc |
| 650 #7 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Aerospace & aviation technology |
| Source of heading or term |
thema |
| 830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE |
|---|
| Uniform title |
Elsevier aerospace engineering series. |
| 856 41 - ELECTRONIC LOCATION AND ACCESS |
|---|
| Link text |
View Publisher Description |
| Uniform Resource Identifier |
<a href="http://store.elsevier.com/product.jsp?isbn=9781856179126">http://store.elsevier.com/product.jsp?isbn=9781856179126</a> |
| 856 41 - ELECTRONIC LOCATION AND ACCESS |
|---|
| Link text |
Send a message to library staff if access to this online resource is unavailable |
| Uniform Resource Identifier |
<a href="mailto:libdesk@itcarlow.ie?subject=Resource%20unavailable">mailto:libdesk@itcarlow.ie?subject=Resource%20unavailable</a> |
| 902 ## - LOCAL DATA ELEMENT B, LDB (RLIN) |
|---|
| a |
170601 |
| 907 ## - LOCAL DATA ELEMENT G, LDG (RLIN) |
|---|
| a |
.b10411136 |
| b |
cgen |
| c |
- |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Suppress in OPAC |
0 |
| 998 ## - LOCAL CONTROL INFORMATION (RLIN) |
|---|
| Operator's initials, OID (RLIN) |
0 |
| Cataloger's initials, CIN (RLIN) |
120530 |
| First Date, FD (RLIN) |
m |
| Local |
a |
| -- |
- |
| -- |
0 |