The addition of quasi-three-dimensional terms into a finite element method for transonic turbomachinery blade-to-blade flows

Author:

Cedar R. D.,Stow P.

Publisher

Wiley

Subject

Applied Mathematics,Computer Science Applications,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference6 articles.

1. ‘A general theory of three-dimensional flow in subsonic and supersonic turbomachines of axial-, radial- and mixed-flow types’, NACA TN 2604, 1952.

2. and ‘Force and moment coefficients for high deflection cascades’, Cambridge University Engineering Department Report CUED/A-Turbo/TR 98, 1980.

3. and , ‘A finite element method for the solution of two-dimensional transonic and supersonic flows’. To be published in International Journal for Numerical Methods in Fluids.

4. ‘Boundary layer transition and separation at the leading edge of a high speed turbine blade’, ASME PAPER 84-GT-241, June 1984.

5. Rolls-Royce Turbine Department, private communication.

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Fluid-Structural Coupling Effects on the Dynamics of Mistuned Bladed Disks;AIAA Journal;2007-03

2. REDUCED-ORDER MODELS OF UNSTEADY TRANSONIC VISCOUS FLOWS IN TURBOMACHINERY;Journal of Fluids and Structures;2000-11

3. Prediction of Unsteady 2D-Flow in Turbomachinery Bladings;Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines and Propellers;1993

4. A finite element solution of unsteady two-dimensional flow in cascades;International Journal for Numerical Methods in Fluids;1990-01-05

5. The role of a mixed design and analysis method in a turbomachinery blade design system;Communications in Applied Numerical Methods;1986-01

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