000			02888nam a22003975i 4500
710	2		_aSpringerLink (Online service) _0http://id.loc.gov/authorities/names/no2005046756 _1http://viaf.org/viaf/274647764/ _9106996
999			_c102362 _d102362 _x1
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005			20230102113038.0
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007			cr nn 008mamaa
008			180503s2018 gw | s |||| 0|eng d
020			_a9783319762432
024	7		_a10.1007/978-3-319-76243-2 _2doi
040			_bspa _cES-MaUEC _dES-MaUEC
050		4	_aTL709 _b2018 EB
100	1		_aBiswas, Sayan _9673388
245	1	0	_aPhysics of Turbulent Jet Ignition : _bMechanisms and Dynamics of Ultra-lean Combustion _cby Sayan Biswas
264		1	_aCham _bSpringer International Publishing _c2018
300			_a1 recurso en línea (XVIII, 216 páginas) _b131 ilustraciones, 108 ilustraciones a color
336			_2rdacontent _aTexto _btxt
337			_2rdamedia _aelectrónico _bc
338			_2rdacarrier _arecurso electrónico _bcr
347			_atext file _bPDF
490	0		_aSpringer Theses, Recognizing Outstanding Ph.D. Research, _x2190-5053
490	0		_aEngineering (Springer-11647)
505	0		_aIntroduction -- 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	3		_aThis 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.
988			_aEBSPRINGER_2018
650		7	_2embne _9189176 _aAviones _xMotores
776	0	8	_iEdición impresa: _z9783319762425
776	0	8	_iEdición impresa: _z9783319762449
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-3-319-76243-2 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
942			_2lcc _cLE
998			_b04/2020 _dz _eu _zSI