An inverse blade design method for subsonic and transonic viscous flow in compressors and turbines
Author:
Affiliation:
1. Department of Mechanical and Industrial Engineering Concordia University, Montreal, Quebec, H3G 1M8, Canada
Publisher
Informa UK Limited
Subject
Applied Mathematics,Computer Science Applications,General Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/17415970500354235
Reference19 articles.
1. Designing turbomachinery blades with the function approximation concept and the Navier-Stokes equations
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5. Finite Element Formulation for Two-Dimensional Inverse Heat Conduction Analysis
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