Unified aerodynamic-acoustic theory for a thin rectangular wing encountering a gust

DOI10.2514/3.7675zbMath0429.76009OpenAlexW2132675498MaRDI QIDQ3867386

Rudolph Martinez, Sheila E. Widnall

Publication date: 1980

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

Full work available at URL: https://doi.org/10.2514/3.7675

zbMATH Keywords

subsonicleading- and trailing-edge responsesstationary short-wavelength oblique gustthin rectangular wingtwo- dimensional pressure fieldunified aerodynamic-acoustic theory

Mathematics Subject Classification ID

Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

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