Integral Equation Method for Subsonic Flow Past Airfoils in Ventilated Wind Tunnels

DOI10.2514/3.49629zbMath0323.76007OpenAlexW1634350261MaRDI QIDQ4086854

M. Mokry

Publication date: 1975

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.49629

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Related Items (2)

The application of the boundary integral equations method to subsonic flow with circulation past thin airfoils in a wind tunnel ⋮ Exact solution for wind tunnel interference using the panel method

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