A compatible mixed design and analysis finite element method for the design of turbomachinery blades
Abstract
In this paper the development of a compatible mixed design and analysis method is presented for the quasi-three-dimensional finite element blade-to-blade program FINSUP. The method consists of two parts. The first is concerned with a method of modeling changes to a blade shape using a surface transpiration model. The second is concerned with determining the relationship between the displaced blade surface and the surface velocity distribution. It is shown that with the Newton-Raphson procedure adopted in the method a very efficient manner of introducing the design option is possible. As a consequence the resulting program is fast and completely interactive. A number of examples are given to illustrate how the mixed design and analysis mode can be used in practical blade design.
- Publication:
-
International Journal for Numerical Methods in Fluids
- Pub Date:
- April 1985
- DOI:
- Bibcode:
- 1985IJNMF...5..331C
- Keywords:
-
- Compressor Blades;
- Computational Fluid Dynamics;
- Computer Aided Design;
- Finite Element Method;
- Newton-Raphson Method;
- Turbine Blades;
- Cascade Flow;
- Mach Number;
- Mass Flow;
- Mathematical Models;
- Surface Geometry;
- Transonic Compressors;
- Transpiration;
- Turbomachinery;
- Fluid Mechanics and Heat Transfer