Numerical study of improving aerodynamic performance of low solidity LPT cascade through increasing trailing edge thickness
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-016-0869-4.pdf
Reference22 articles.
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2. Praisner T J, Grover E A, Knezevici D C, et al. Toward the expansion of low-pressure-turbine airfoil design space. ASME Paper GT2008-50898, Berlin, Germany.
3. Gier J, Franke M, Hubner N, et al. Designing LP turbines for optimized airfoil lift, ASME Paper GT2008-51101, Berlin, Germany.
4. Chen PP, QIAO WY, Luo HL, et al. Investigation of Low Solidity LP Turbine Cascade With Flow Control: Part 1-Active Flow Control Using Jet-Flap. ASME Paper GT2010-22328, Glasgow, UK.
5. Lake JP, King PI, Rivir RB. Low Reynolds number loss reduction on turbine blades with dimples and V-grooves. AIAA 2000-0738, Reno, Nevada.
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