Numerical optimization for turbomachinery blades aerodynamic design using a gradient method coupled with Navier-Stokes solver

Burguburu, Stephane
Toussaint, Clement
Leroy, Gilles
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

Publication date

January 2001

Abstract

Communication to : 15th international symposium on airbreathing engines, Bangladore (Inde), September 02-07, 2001SIGLEAvailable from INIST (FR), Document Supply Service, under shelf-number : 22419, issue : a.2001 n.190 / INIST-CNRS - Institut de l'Information Scientifique et TechniqueFRFranc

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Numerical optimization for turbomachinery blades aerodynamic design using a gradient method coupled with Navier-Stokes solver

Abstract

Extracted data

Numerical optimization for turbomachinery blades aerodynamic design using a gradient method coupled with Navier-Stokes solver

Abstract

Extracted data

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