The Influence of a Nonzero Angle of Attack and Gust Loads on the Nonlinear Response of a Typical Airfoil Section with a Control Surface Freeplay
DOI10.1515/IJNSNS.2000.1.3.153zbMath0965.76012MaRDI QIDQ4503835
Denis B. Kholodar, Earl. H. Dowell
Publication date: 21 November 2000
Published in: International Journal of Nonlinear Sciences and Numerical Simulation (Search for Journal in Brave)
nonlinear dynamicsangle of attackpressure distributionstructural dampingWagner functionaeroelastic wingthree-degree-of-freedom airfoil sectionlow speed wind tunnelcontrol surface freeplayDuhamel's superposition integralgust generatorharmonic gust excitationJones' approximationNACA 0012 rectangular wing modelquenching effectSchwarz's solutionTheodorsen aerodynamics
Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)
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