Japan Aerospace Exploration Agency Aviation Program Group
Japan Aerospace Exploration Agency Aviation Program Group
Japan Aerospace Exploration Agency Aviation Program Group
Japan Aerospace Exploration Agency Aviation Program Group
Experimental study of film cooling, impingement cooling and integrated cooling were carried out with the aim of applying them to turbine cooling. The experiments were conducted with 673 K hot gas flow and room temperature cooling air. Test plate surface temperature distributions were measured with an infrared camera. This report presents fundamental research data on cooling performance of the test plates for the validation of numerical simulation. Moreover, simplify heat transfer calculations were executed and were evaluated by the experimental measurements.
複合冷却方式タービン翼の冷却性能に関する研究
63461000.pdf
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