Transonic Panel Method to Determine Loads on Oscillating Airfoils with Shocks

DOI10.2514/3.50977zbMath0455.76064OpenAlexW2039403865MaRDI QIDQ3904271

Michael H. L. Hounjet

Publication date: 1981

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

Full work available at URL: https://doi.org/10.2514/3.50977

zbMATH Keywords

oscillating airfoilseffect of moving shocklinear lifting surface theoriesLTRAN 2 codeNACA 64A006 airfoilvelocity potential panel approach

Mathematics Subject Classification ID

Transonic flows (76H05) Applications to the sciences (65Z05) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Related Items (1)

Development of a shock-fitting field-panel method for 3D transonic flows

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