Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine--Part II: Effect of Cooling Variation on the Vane Airfoil and Inner End Wall.
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| Title: | Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine--Part II: Effect of Cooling Variation on the Vane Airfoil and Inner End Wall. |
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| Authors: | Kahveci, Harika S.1, harika.kahveci@ge.com, Haldeman, Charles W.1, haldeman.5@osu.edu, Mathison, Randall M.1, mathison.4@osu.edu, Dunn, Michael G.1, dunn.129@osu.edu |
| Source: | Journal of Turbomachinery; Mar2013, Vol. 135 Issue 2, p1-8, 8p |
| Database: | Applied Science & Technology Source |
| ISSN: | 0889504X |
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| DOI: | 10.1115/1.4006776 |
