The role of a mixed design and analysis method in a turbomachinery blade design system

DOI10.1002/CNM.1630020113zbMath0591.76087OpenAlexW2048420950MaRDI QIDQ3720121

R. D. Cedar, P. Stow

Publication date: 1986

Published in: Communications in Applied Numerical Methods (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/cnm.1630020113

zbMATH Keywords

Newton-Raphson procedureturbomachinery blade designsurface transpiration modelblade shapeblade with controlled suction surface diffusionfinite element blade- to-blade methodmulti-stage compressorsquasi three- dimensional compatible design and analysis methodsuction surface shocktransonic compressor blade

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Basic methods in fluid mechanics (76M99)

Related Items (1)

Computational methods for aerodynamic shape design

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