Application of elliptic continuation method for transonic aerofoil design and experimental verification

DOI10.1002/NME.1620220208zbMath0591.76100OpenAlexW2135910407MaRDI QIDQ3720144

G. Wichmann, H.-Chr. Oelker, G. Redeker

Publication date: 1986

Published in: International Journal for Numerical Methods in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/nme.1620220208

zbMATH Keywords

design processelliptic continuation methodhigher design Mach numbershigher lift coefficientsshock-free pressure distributionstransonic aerofoils

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Transonic flows (76H05) Basic methods in fluid mechanics (76M99)

Related Items (1)

Computational methods for aerodynamic shape design

Cites Work

• Supercritical wing sections II. A handbook
• Supercritical wing sections. III

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