Optimal Design of Rotor Blades for an Axial Compressor Using the Gradient Based Method
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Publisher
Springer International Publishing
Link
http://link.springer.com/content/pdf/10.1007/978-3-319-97773-7_45
Reference14 articles.
1. Marshall, J.G., Imregun, M.: A review of aeroelasticity methods with emphasis on turbomacinery applications. J. Fluids Struct. 10(3), 237–267 (1996)
2. Hicks, R.M., Henne, P.A.: Wing design by numerical optimization. J. Aircr. 15(7), 407–412 (1978)
3. Kammerer, S., Mayer, J.F., Paffrath, M., Wever, U., Jung, A.R.: Three-dimensional optimization of turbomachinery bladings using sensitivity analysis. In: ASME Turbo Expo, GT2003-38037 (2003)
4. Catalano, L.A., Dadone, A.: Orthogonal shape functions and progressive optimization for the design of 2-D transonic cascades. In: Proceedings of ASME Turbo Expo 2002, GT-2002-30678 (2002)
5. Reynolds, O.: On the dynamical theory of incompressible viscous fluids and the determination of the criterion. Philos. Trans. R. Soc. Lond. A 186, 123–164 (1895)
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