Subsonic flow past a thin airfoil in a wind tunnel

DOI10.1016/0093-6413(91)90041-TzbMath0722.76034OpenAlexW2067276810MaRDI QIDQ756546

Lazăr Dragoş

Publication date: 1991

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

Full work available at URL: https://doi.org/10.1016/0093-6413(91)90041-t

zbMATH Keywords

numerical methodsubsonic flowwind tunnelintegral equation of a thin airfoil

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25)

Related Items (1)

The application of the boundary integral equations method to subsonic flow with circulation past thin airfoils in a wind tunnel

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