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scientific article; zbMATH DE number 1341564 - MaRDI portal

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Publication:4263107

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zbMath0930.76042MaRDI QIDQ4263107

Susumu Takanashi, Kisa Matsushima

Publication date: 14 February 2000

Title: zbMATH Open Web Interface contents unavailable due to conflicting licenses.

zbMATH Keywords

supersonic wing iterative design target pressure distribution residual-correction loop transonic wing wing section shape

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Supersonic flows (76J20)

Related Items (1)

Inverse shape design method based on pressure and shear stress for separated flow via Elastic Surface Algorithm

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