Coverart for item
The Resource Aircraft propulsion and gas turbine engines, Ahmed F. El-Sayed

Aircraft propulsion and gas turbine engines, Ahmed F. El-Sayed

Label
Aircraft propulsion and gas turbine engines
Title
Aircraft propulsion and gas turbine engines
Statement of responsibility
Ahmed F. El-Sayed
Creator
Author
Subject
Language
eng
Summary
"AIRCRAFT PROPULSION and GAS TURBINE ENGINES, Second Edition, will be a significantly updated and expanded survey of today's aeronautical and aerospace propulsion. The book will be divided into three parts rather than two as in its 1st edition. The first two parts are devoted to air breathing engines, while the third part will handle non-air breathing or rocket engines. The first part investigates the performance of air/land gas turbines, while the second part deals with the description, analysis and design of gas turbine modules. This edition will exhibit major and minor changes compared with 1st edition. Major changes include the adding of three new topics; namely, piston engines together with integrated propeller coverage; pumps; and rocket propulsion. Rocket propulsion has been added, to serve courses that include aerospace topics as well as aircraft. A complete Solutions Manual and Exam Supplement will be available for qualified adopting instructors"--Provided by publisher
Cataloging source
PSt/DLC
http://library.link/vocab/creatorName
El-Sayed, Ahmed F
Dewey number
629.134/353
Illustrations
illustrations
Index
index present
LC call number
TL709
LC item number
.E42 2017
Literary form
non fiction
Nature of contents
bibliography
http://library.link/vocab/subjectName
  • Airplanes
  • Aircraft gas-turbines
  • Aircraft gas-turbines
  • Airplanes
Label
Aircraft propulsion and gas turbine engines, Ahmed F. El-Sayed
Instantiates
Publication
Bibliography note
Includes bibliographical references and index
Carrier category
volume
Carrier category code
  • nc
Carrier MARC source
rdacarrier
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent
Contents
History and classifications of aero-engine -- Performance parameters of jet engines -- Pulsejet and ramjet engines -- Turbojet engine -- Turbofan engines -- Shaft engines -- High speed supersonic and hypersonic engines -- Industrial gas turbines -- Power plant installation and intakes -- Combustion systems -- Exhaust system -- Centrifugal compressors -- Axial flow compressors and fans -- Axial turbines -- Radial inflow turbines -- Module matching -- Selected topics -- Introduction to rocketry -- Rocket engines
Control code
974212089
Dimensions
27 cm
Edition
Second edition.
Extent
xxvii, 1,447 pages
Isbn
9781466595163
Lccn
2016048776
Media category
unmediated
Media MARC source
rdamedia
Media type code
  • n
Other physical details
illustrations
System control number
(OCoLC)974212089
Label
Aircraft propulsion and gas turbine engines, Ahmed F. El-Sayed
Publication
Bibliography note
Includes bibliographical references and index
Carrier category
volume
Carrier category code
  • nc
Carrier MARC source
rdacarrier
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent
Contents
History and classifications of aero-engine -- Performance parameters of jet engines -- Pulsejet and ramjet engines -- Turbojet engine -- Turbofan engines -- Shaft engines -- High speed supersonic and hypersonic engines -- Industrial gas turbines -- Power plant installation and intakes -- Combustion systems -- Exhaust system -- Centrifugal compressors -- Axial flow compressors and fans -- Axial turbines -- Radial inflow turbines -- Module matching -- Selected topics -- Introduction to rocketry -- Rocket engines
Control code
974212089
Dimensions
27 cm
Edition
Second edition.
Extent
xxvii, 1,447 pages
Isbn
9781466595163
Lccn
2016048776
Media category
unmediated
Media MARC source
rdamedia
Media type code
  • n
Other physical details
illustrations
System control number
(OCoLC)974212089

Library Locations

    • Curtis Laws Wilson LibraryBorrow it
      400 West 14th Street, Rolla, MO, 65409, US
      37.955220 -91.772210
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