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10篇 您的检索式:作者名="Dorignac"
    题名 作者 年代 出处 被引量
1Ultra-high resolution electron microscopy investigation of growth defects in CVD diamond films:twin interaction and fivefold twin centers显示文摘Delclos S Dorignac D Phillipp F 2000Diamond Relat Mater2000,9,:1
2An experimental study on hot round jets impinging a concave surface显示文摘M. Fenot E. Dorignac J.-J. Vullierme 2008International Journal of Heat and Fluid Flow2008,,4:1
3Convective Heat Transfer in the Entry Region of an Annular Channel 显示文摘Fenot M Dorignac E Giret A 2013Applied ThermM Engineering2013,,54:1
4An Experimental Study on Hot Round Jets Impinging a Concave Surface 显示文摘Fenot M Dorignac E Vullierme J J 2008International Journal of Heat and Fluid Flow2008,29,4:1
5Heat Transfer to a Row of Impinging Jets in Consideration of Optimization显示文摘BREVET P DEJEU C DORIGNAC E 2002In- ternational Journal of Heat and Mass Transfer2002,45,20:1
6HREM and EXELFS investigation of local structure in thin CVD diamond films显示文摘Dorignac D Serin V Delclos S 1997Diamond and Related Materials1997,6,:1
7Heattransfer to a row of impinging jets in consideration ofoptimization 显示文摘Brevet P Dorignac C Jolly M Vullierme J J 2002Heat and Mass Transfer2002,45,:1
8HREM and EXELFS investigation of local structure in thin CVD diamond films显示文摘Dorignac D Serin V Delclos S 1997Diamond Relat Mater1997,6,:1
9Study of Several Impinging Jets显示文摘Impinging jets are frequently adapted for cooling overheated parts. With the film cooling technique, this process improves thermal exchanges between walls and fluid. However if many works have concerned only the thermal aspect of this problem [1], its dynamic field has been rarely studied especially for multiple impingements. As the two phenomena cannot be totally dissociated, we have undertaken the aerodynamic and thermal study of jets impinging on a plane wall. Various techniques have been used as visualizations (spreading over method, LASER sheet visualizations), LDA measurements to propose a topology schema of the flow and infrared thermography.L.-Emmanuel BRIZZI Anthony BERNARD J.-Louis BOUSGARBIES Eva DORIGNAC J. -Jacques VULLIERME (Laboratoire d’Etudes Aerodynamiques (UMR 6609), Boulevard 3, Teleport 2, BP 179, 86960 FUTUROSCOPE Cedex. France. Laboratoire de Mecanique de Lille (URA 1441 2000Journal of Thermal Science2000,9,3:0
10Heat Transfer Model with Two Heat Transfer Coefficients Along a M ultiperforated Plate-Application to Combustion Chamber Wall Cooling显示文摘Walls' cooling of aeronautic propeller combustion chamber is performed with the injection, through the combustion chamber wall, of a part of the air coming from compressors placed upstream. Measurements of the wall thermal fields are made by infrared thermography along the injection wall. This injection wall is pierced by 9 rows of 8 holes (α=90°) in staggered configuration (p/D=s/D=6). We propose a model using two heat transfer coefficients to represent the convective exchanges. The results are non-dimensioned and presented in comparison with the case without holes. The use of this model allows us to define 4 zones. Those 4 zones exist for the 5 blowing rates.Brice Petre Eva Dorignac Jean Jacques Vullierme 2003Journal of Thermal Science2003,12,4:0
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