Aerodynamic inverse design of turbomachinery blading in two-dimensional viscous flow

An inverse blade design method, applicable to 2D and 3D flow in turbomachinery blading is developed and is implemented for the design of 2D cascades in compressible viscous flow. The prescribed design quantities are either the pressure distributions on the blade suction and pressure surfaces or the...

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Bibliographic Details
Main Author: Daneshkhah, Kasra
Format: Others
Published: 2006
Online Access:http://spectrum.library.concordia.ca/8925/1/NR16295.pdf
Daneshkhah, Kasra <http://spectrum.library.concordia.ca/view/creators/Daneshkhah=3AKasra=3A=3A.html> (2006) Aerodynamic inverse design of turbomachinery blading in two-dimensional viscous flow. PhD thesis, Concordia University.