[1] Yanovske L S. Physical Basis of Transpiration Cooling for Engines of Flying Apparatus[M].Moscow: MAI Press, 1996.
[2] Mueggenburg H H, Hidahl J W, Kessler E L. Platelet Actively Cooled Thermal Management Devices[R].AIAA 92-3127.
[3] Terry J E, Caras G J. Transpiration and Film Cooling of Liquid Rocket Nozzles[R].AD-486409, 1966.
[4] Haeseler D, Mading C, Rubinskiy V, et al. Experimental Investigation of Transpiration Cooled Hydrogen-Oxygen Subscale Chambers[R].AIAA 98-3664.
[5] Serbest E, Haidn O, Hald H, et al. Effusion Cooling in Rocket Combustors Applying Fiber Reinforced Ceramics[R].AIAA 99-2911.
[6] Bartle E R, Leadon B M. The Effectiveness as a Universal Measure of Mass Transfer Cooling for a Turbulent Boundary Layer[C].California: Proceedings of the 1962 Heat Transfer and Fluid Mechanics Institute, Stanford University Press, 1962.
[7] Kays W M, Crawford M E. Convective Heat and Mass Transfer[M].New York: McGraw-Hill Inc., 1993.
[8] Rannie W D. A Simplified Theory of Porous Wall Cooling[M].Pasadena: Jet Propulsion Laboratory California Institute of Technology, 1947.
[9] Laganelli L. Comparison between Film Cooling and Transpiration Cooling System in High Speed Flow[R].AIAA 70-153.
[10] Wheeler H L, Duwez P. Heat Transfer Through Sweat Cooled Porous Tubes[J].Jet Propulsion, 1955, 25(1).
[11] Chen F, Bowman W J, Bowersox R. Effect of Transpiration Cooling on Nozzle Heat Transfer[J].J.Spacecraft, 1995, 33(3): 453-455 .
[12] Meinert J, Huhn J, Serbest E, et al. Turbulent Boundary Layers with Foreign Gas Transpiration[J].J.of Spacecraft and Rockets, 2001, 38(2).
[13] Lezuo M, Haidn O J. Transpiration Cooling in H2/O2-Combustion Devices[R]. AIAA 96-2581.
[14] Frohlke K, Haidn O, Serbest E. New Experimental Results on Transpiration Cooling for H2/O2 Rocket Combustion Chambers[R]. AIAA 98-3443.
[15] May L R, Burkhardt W M. Transpiration Cooled Throat for Hydrocarbon Rocket Engines[R].AD-A244255, 1991.
[16] Greuel D, Herbertz A, Haidn O J, et al. Transpiration Cooling Applied to C/C Liners of Cryogenic Liquid Rocket Engines[R]. AIAA 2004-3682.
[17] Tang J, Chen Y F, Sun J G, et al. Properties and Application of Oriented Porous SiC as Transpiration Cooling Materials[C]. Chengdu: The 4th China International Conference on High Performance Ceramics, 2005.
[18] Keener D, Lenertz J, Bowersox R, et al. Transpiration Cooling Effects on Nozzle Heat Transfer and Performance[J]. J.of Spacecraft and Rockets, 1995, 32(6).(编辑:梅瑛) * 收稿日期:2013-10-15;修订日期:2014-03-26。作者简介:李青(1967—),男,硕士,副教授,研究领域为热能动力设备与应用领域教学与科研工作。E-mail:gylq206@sina.com
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