Aerodynamic loading distribution effects on the overall performance of ultra-high-lift LP turbine cascades
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-014-0671-0.pdf
Reference22 articles.
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2. Mayle R. E., (1991), The Role of Laminar-Turbulent Transition in Gas Turbine Engines, ASME Journal of Turbomachinery, Vol. 113, pp. 509–531.
3. Hodson, H. P., and Howell, R.J., (2005), The Role of Transition in High-Lift Low-Pressure Turbines for Aeroengines, Progress in Aerospace Sciences, Vol. 41, pp. 419–454.
4. Simoni, D., Ubaldi, M., Zunino, P., Lengani, D., Bertini, F., (2012), An Experimental Investigation of the Separated-Flow Transition Under High-Lift Turbine Blade Pressure Gradients, Flow Turbulence and Combustion, Vol. 88(1–2), pp. 45–62.
5. Simoni, D., Ubaldi, M., Zunino, P., (2012), Loss Production Mechanisms in a Laminar Separation Bubble, Flow Turbulence and Combustion, Vol. 89, pp. 547–562.
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