论文信息 - Arbitrary Blade Section Design Based on Viscous Considerations. Background Information

Arbitrary Blade Section Design Based on Viscous Considerations. Background Information

Background information is presented on an arbitrary blade section design method which is outlined in a joint paper. This information concerns the assumptions, the development, and the predictive capabilities of the viscous flow calculation tool used in the design procedure. General properties of laminar and turbulent, unseparated or separated compressible shear layers, necessary for the blade optimization procedure, are discussed.

[1] K. D. Papailiou,et al. An Inverse Inviscid Method for the Design of Quasi-Three-Dimensional Turbomachinery Cascades , 1993 .

[2] K. D. Papailiou,et al. Transition Prediction in Attached and Separated Shear Layers Using an Integral Method , 1992 .

[3] H. B. Keller,et al. Shooting and parallel shooting methods for solving the Falkner-Skan boundary-layer equation , 1971 .

[4] K. D. Papailiou,et al. The Behaviour of the Normal Fluctuation Terms in the Case of Attached or Detached Turbulent Boundary Layers , 1984 .

[5] K. Stewartson,et al. Correlated incompressible and compressible boundary layers , 1949, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.

[6] Jack N. Nielsen,et al. Prediction of turbulent separated boundary layers , 1973 .

[7] H. Schlichting. Boundary Layer Theory , 1955 .

[8] K. D. Papailiou,et al. An Integral Method for Calculating Turbulent Boundary Layer With Separation , 1979 .