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International Journal of Rotating Machinery
Volume 6, Issue 5, Pages 313-319
http://dx.doi.org/10.1155/S1023621X00000294

Turbine Airfoil Leading Edge Film Cooling Bibliography: 1972–1998

GE Aircraft Engines, M/S 240-GH, 1000 Western Ave., Lynn 01910, MA, USA

Received 10 March 1999; Revised 7 May 1999

Copyright © 2000 Hindawi Publishing Corporation. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Citations to this Article [8 citations]

The following is the list of published articles that have cited the current article.

  • Y.-L. Lin, and T. I.-P. Shih, “Film Cooling of a Cylindrical Leading Edge With Injection Through Rows of Compound-Angle Holes,” Journal of Heat Transfer, vol. 123, no. 4, pp. 645, 2001. View at Publisher · View at Google Scholar
  • Michael G. Dunn, “Convective Heat Transfer and Aerodynamics in Axial Flow Turbines,” Journal of Turbomachinery, vol. 123, no. 4, pp. 637, 2001. View at Publisher · View at Google Scholar
  • Gottfried Laschet, Stephan Rex, Dieter Bohn, and Robert Krewinkel, “Three-Dimensional Numerical Analysis of Curved Transpiration Cooled Plates and Homogenization of Their Aerothermal Properties,” Journal of Turbomachinery, vol. 129, no. 4, pp. 791, 2007. View at Publisher · View at Google Scholar
  • C. W. Haldeman, R. M. Mathison, M. G. Dunn, S. A. Southworth, J. W. Harral, and G. Heitland, “Aerodynamic and Heat Flux Measurements in a Single-Stage Fully Cooled Turbine—Part I: Experimental Approach,” Journal of Turbomachinery, vol. 130, no. 2, pp. 021015, 2008. View at Publisher · View at Google Scholar
  • James D. Heidmann, and Srinath Ekkad, “A Novel Antivortex Turbine Film-Cooling Hole Concept,” Journal of Turbomachinery, vol. 130, no. 3, pp. 031020, 2008. View at Publisher · View at Google Scholar
  • Harika S. Kahveci, “Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine—Part I: Experimental Configuration and Data Review With Inlet Temperature Profile Effects,” Journal of Turbomachinery, vol. 135, no. 2, pp. 021027, 2012. View at Publisher · View at Google Scholar
  • C. W. Haldeman, M. G. Dunn, and R. M. Mathison, “Fully Cooled Single Stage HP Transonic Turbine—Part I: Influence of Cooling Mass Flow Variations and Inlet Temperature Profiles on Blade Internal and External Aerodynamics,” Journal of Turbomachinery, vol. 134, no. 3, pp. 031010, 2012. View at Publisher · View at Google Scholar
  • Yongbin Ji, Bing Ge, Zhongran Chi, and Shusheng Zang, “Overall Cooling Effectiveness of Effusion Cooled Annular Combustor Liner at Reacting Flow Conditions,” Applied Thermal Engineering, 2017. View at Publisher · View at Google Scholar