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Showing 1 to 2 of 2 for “"Equivalent Plate Model"”.
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Efficient Methods for Structural Analysis of Built-Up Wings
… the conclusion that physics-based high-fidelity models need to be used as early as possible in the design of its products. At the preliminary design stage of wing structures, though highly desirable for its high accuracy, a detailed finite element analysis(FEA) is often not feasible due to the …
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Sensitivity analysis of wing aeroelastic responses
… forces on a wing. This is coupled with an equivalent plate structural model based on a Rayleigh-Ritz formulation and the aeroelastic equations are solved as an eigenvalue problem to determine the critical speed of the wing. The sensitivity of divergence and flutter speeds to shape …