Effect of Leading-Edge Optimization on the Loss Characteristics in a Low-Pressure Turbine Linear Cascade
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-019-1196-3.pdf
Reference35 articles.
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3. Hodson, H.P., Boundary-layer transition and separation near the leading edge of a high-speed turbine blade. ASME Journal of Engineering for Gas Turbines and Power, 1985, 107(1): 127–134.
4. Ward, J.W., The behavior and effects of laminar separation bubbles on aerofoils in incompressible flow. Journal of the Royal Aeronautical Society, 1963, 67(636): 783–790.
5. Crimi, P., Reeves, B.L., Analysis of leading-edge separation bubbles on airfoils. AIAA Journal, 1976, 14(11): 1548–1555.
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