Physics of Turbulent Jet Ignition (Record no. 78720)

000 -LEADER
fixed length control field 03394nam a22005775i 4500
001 - CONTROL NUMBER
control field 978-3-319-76243-2
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20220801220601.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 180503s2018 sz | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9783319762432
-- 978-3-319-76243-2
082 04 - CLASSIFICATION NUMBER
Call Number 629.1
100 1# - AUTHOR NAME
Author Biswas, Sayan.
245 10 - TITLE STATEMENT
Title Physics of Turbulent Jet Ignition
Sub Title Mechanisms and Dynamics of Ultra-lean Combustion /
250 ## - EDITION STATEMENT
Edition statement 1st ed. 2018.
300 ## - PHYSICAL DESCRIPTION
Number of Pages XVIII, 216 p. 131 illus., 108 illus. in color.
490 1# - SERIES STATEMENT
Series statement Springer Theses, Recognizing Outstanding Ph.D. Research,
505 0# - FORMATTED CONTENTS NOTE
Remark 2 Introduction -- Ignition Mechanisms -- Schlieren Image Velocimetry (SIV) -- Supersonic Jet Ignition -- Combustion Instability at Lean Limit -- Ignition by multiple turbulent jets -- Impinging Jet Ignition -- Flame Propagation in Microchannels -- Summary and outlook -- Appendix -- Conclusion.
520 ## - SUMMARY, ETC.
Summary, etc This book focuses on developing strategies for ultra-lean combustion of natural gas and hydrogen, and contributes to the research on extending the lean flammability limit of hydrogen and air using a hot supersonic jet. The author addresses experimental methods, data analysis techniques, and results throughout each chapter and: Explains the fundamental mechanisms behind turbulent hot jet ignition using non-dimensional analysis Explores ignition characteristics by impinging hot jet and multiple jets in relation to better controllability and lean combustion Explores how different instability modes interact with the acoustic modes of the combustion chamber. This book provides a potential answer to some of the issues that arise from lean engine operation, such as poor ignition, engine misfire, cycle-to-cycle variability, combustion instability, reduction in efficiency, and an increase in unburned hydrocarbon emissions. This thesis was submitted to and approved by Purdue University.
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier https://doi.org/10.1007/978-3-319-76243-2
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type eBooks
264 #1 -
-- Cham :
-- Springer International Publishing :
-- Imprint: Springer,
-- 2018.
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-- computer
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-- rdamedia
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-- online resource
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-- text file
-- PDF
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650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Astronautics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Fluid mechanics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Renewable energy sources.
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace Technology and Astronautics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engineering Fluid Dynamics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Renewable Energy.
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE
-- 2190-5061
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-- ZDB-2-ENG
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