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6篇 您的检索式：作者名="Laskaridis"

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		题名	作者	年代	出处	被引量
	1	Proximate composition,fatty acid analysis and protein digestibilitycorrected amino acid score of three Mediterranean cephalopods显示文摘	Zlatanos S Laskaridis K Feist C Sagredos A		0，，：	1
	2	CLA content and fatty acid composition of Greek Feta and hard cheeses显示文摘	ZLATANOS S LASKARIDIS K FEIST C	2002	Food Chemistry2002，78，：	1
	3	Investigation into the effects of operating conditions and design parameters on the creep life of high pressure turbine blades in a stationary gas turbine engine显示文摘	Eshati S Laskaridis P	2011	Mechanics and Mechanical Engineering2011，15，3：	1
	4	Aero-engine turbine blade life assessment using the Neu/Sehitoglu damage modei显示文摘	Abu A O Eshati S Laskaridis P	2014	IntemationaI Joumal of Fatigue2014，，61：	1
	5	Influence of water-air ratio on the heat transfer and creep life of a high pressure gas turbine blade显示文摘	Eshati S Abu A Laskaridis P	2013	Applied Thermal Engineering2013，60，12：	1
	6	Discretized Miller approach to assess effects on boundary layer ingestion induced distortion显示文摘The performance of propulsion configurations with boundary layer ingestion(BLI) is affected to a large extent by the level of distortion in the inlet flow field. Through flow methods and parallel compressor have been used in the past to calculate the effects of this aerodynamic integration issue on the fan performance; however high-fidelity through flow methods are computationally expensive, which limits their use at preliminary design stage. On the other hand, parallel compressor has been developed to assess only circumferential distortion. This paper introduces a discretized semi-empirical performance method, which uses empirical correlations for blade and performance calculations. This tool discretizes the inlet region in radial and circumferential directions enabling the assessment of deterioration in fan performance caused by the combined effect of both distortion patterns. This paper initially studies the accuracy and suitability of the semiempirical discretized method by comparing its predictions with CFD and experimental data for a baseline case working under distorted and undistorted conditions. Then a test case is examined,which corresponds to the propulsor fan of a distributed propulsion system with BLI. The results obtained from the validation study show a good agreement with the experimental and CFD results under design point conditions.	Esteban Valencia Víctor Hidalgo Devaiah Nalianda Laskaridis Panagiotis Riti Singh	2017	Chinese Journal of Aeronautics2017，30，1：	1

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