000 01451pam a2200229a 44500
003 OSt
008 160408bc1990 xxu||||| |||| 00| 0 eng d
020 _a0124900550
040 _cIIT Kanpur
041 _aeng
082 _a621.406
_bD46o
245 1 _aDesign of modern turbine combustors
_cedited by A. M. Mellor
260 _aLondon
_bAcademic Press
_c1990
300 _ax, 557p
440 _aCombustion treatise
490 _a/ edited by J. H. Whitelaw
520 _aLower pollutant emissions and broader multifuel flexibility are driving forces for advancing aircraft, vehicular, and industrial engine performance and versatility. Both are inherently connected with the design of the fuel injector and combustor system. The traditional concerns of improving durability and fuel economy over the life of the engine remain additional requirements.**This volume offers a comprehensive treatment of modern practice aimed both at those in the field and newcomers interested in research and development for gas turbine combustors. Detailed description and assessment of a range of combustor design models and methods; specification and evolution of fuels and fuel injectors; system models for fuel effects on engines and airframes Evaluation of laser-based measurement techniques for combustor flow field studies
650 _aTurbines -- Design and construction
650 _aTurbine design
700 _aMellor, A. M. [ed.]
942 _cBK
999 _c329830
_d329830