Finite-Element Approach to Compressor Blade-to-Blade Cascade Analysis
Author:
Affiliation:
1. Concordia University, Montreal, Quebec, Canada
2. Prattand Whitney Aircraft of Canada Ltd., Longueuil, Quebec, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.61205
Reference16 articles.
1. Analysis of Transonic Cascade Flow Using Conf ormal Mapping and Relaxation Techniques
2. Second order accurate calculation of transonic flow over turbomachinery cascades
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1. Three BEM schemes for the calculating of subsonic compressible plane cascade flow;Engineering Analysis with Boundary Elements;1993-01
2. The use of the finite-element method to calculate acoustic fields in inhomogeneous gas flows;USSR Computational Mathematics and Mathematical Physics;1988-01
3. Finite-element stream function solutions of transonic rotational internal and external flows;Numerical Methods for Partial Differential Equations;1985
4. A finite volume method for two-dimensional transonic potential flow through turbomachinery blade rows;International Journal of Heat and Fluid Flow;1983-12
5. Numerical solution of subsonic and transonic cascade flows;International Journal for Numerical Methods in Fluids;1982-10
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