Author:
Haselbach F.,Schiffer H. -P.
Publisher
Springer Science and Business Media LLC
Reference26 articles.
1. Kruse, H. Effects of Hole Geometry, Wall Curvature and Pressure Gradient on Film Cooling Downstream of a Single Row. AGARD Conference Proceedings No.390, 1985
2. Hay, N, Lampard, D, Saluja, C L. Effects of the Condition of the Approach Boundary Layer and of the Mainstream Pressure Gradients on the Heat Transfer Coefficient on Film-Cooled Surfaces. Journal of Engineering for Gas Turbines and Power, 1985, 107: 99–104
3. Teekaram, A J H, Forth, C J P, Jones, T V. Film Cooling in the Presence of Mainstream Pressure Gradients. Transactions of the ASME, 1991, 113: 484–492
4. Schwarz, S G, Goldstein, R J. The Two-Dimensional Behavior of Film Cooling Jets on Concave Surfaces. Journal of Turbomachinery, 1989, 111: 124–130
5. Abuaf, N, Bunker, R, Lee, C P. Heat Transfer and Film Cooling Effectiveness in a Linear Airfoil Cascade. ASME paper 95-GT-3, 1995
Cited by
2 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献