A fast iterative inverse method for turbomachinery blade design

DOI10.1016/J.MECHRESCOM.2009.01.008zbMath1258.76130OpenAlexW2013508241MaRDI QIDQ1939928

Yanyan Li

Publication date: 5 March 2013

Published in: Mechanics Research Communications (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.mechrescom.2009.01.008

zbMATH Keywords

Euler equationscompressible flowinverse methodturbomachineryblade design

Mathematics Subject Classification ID

Flow control and optimization for compressible fluids and gas dynamics (76N25)

Cites Work

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• Solvability condition and its application to fast numerical solution of overposed inverse problems in compressible flows
• Iterative use of a time-marching code for designing turbomachine blade rows
• Role of constraints in inverse design for transonic airfoils

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