By Edited by: Gurrappa Injeti
ISBN-10: 953307146X
ISBN-13: 9789533071466
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Example text
Vol. 14, No. 9, pp. 1005-1012, ISSN: 1226-4865. Leonard O. & Van Den Braembussche, R. (1992). Two-dimensional Transonic aerodynamic design method. Journal of Turbomachinery, Vol. 3, pp. 553-560, ISSN: 0889504X. Lieblein, S. (1960). Incidence and deviation angle correlations for compressor cascades. Trans. ASME Journal of Basic Engineering, Vol. 82, pp. 575–587. Lighthill, M. (1945). A new method of two-dimensional aerodynamic design. Aeronautical research Council RxM 2104. Marsh, H. (1968). A digital computer program for the throughflow fluid mechanics in an arbitrary turbomachine using a Matrix Method.
This was the case even before the current global awareness to the Climate Change problem. Only NOx gas turbine emission was initially regulated in the early 1970s and it was found that injection of water or steam into the combustion zone of the combustor liner did produce the then required low levels of NOx reduction without serious detrimental effects on the gas turbine parts lives or the overall gas turbine cycle performance. However, as more stringent requirements emerged with time, further increase in water/steam approach began to have significant detrimental effects on the gas turbine parts lives and cycle performance, as well increased levels of other emissions besides NOx.
D. (2004). Aerodynamic Design of 3D Compressor Blade Using an Adjoint Method. AlAA Paper 2004-0027. Dang, T. ; Van Rooij, M. & Larosiliere, L. M. (2003). Design of Aspirated Compressor Blades Using Three-Dimensional Inverse Method. NASA/TM—2003-212212. Demeulenaere, A. & Van Den Braembussche, R. A. (1996). Threedimensional inverse method for turbomachinery blading design. ASME paper 96-GT-39. Denton J. D. & Dawes W. N. (1999). Computational fluid dynamics for turbomachinery design. Journal of Mechanical Engineering Science, IMechE Proc.
Gas Turbines by Edited by: Gurrappa Injeti
by Christopher
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