A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.

DOI10.2514/3.5086zbMath0202.26002OpenAlexW2083473180MaRDI QIDQ5599650

Edward Albano, William P. Rodden

Publication date: 1969

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

Full work available at URL: https://doi.org/10.2514/3.5086

Related Items

Numerical simulation of flapping wings using a panel method and a high-order Navier-Stokes solver ⋮ Coupled fluid structure analysis for wing 445.6 flutter using a fast dynamic mesh technology ⋮ Aerodynamic characteristics of pretensioned elastic membrane rectangular sailwings ⋮ Aeroelastic tailoring using fiber orientation and topology optimization ⋮ Aeroelastic interactions between plates and three-dimensional inviscid potential flows ⋮ Structural optimization of an aeroelastically tailored composite flat plate made of woven fiberglass/epoxy ⋮ Flutter analysis including structural uncertainties ⋮ Multi-fidelity modeling framework for nonlinear unsteady aerodynamics of airfoils ⋮ Subcritical and supercritical nonlinear aeroelastic behavior of a morphing wing with bilinear hinge stiffness ⋮ On the remarkable accuracy of the vortex lattice method ⋮ New developments in vibration reduction with actively controlled trailing edge flaps. ⋮ A parallel, object-oriented framework for unsteady free-wake analysis of multi-rotor/wing systems ⋮ Reduced-order fluid/structure modeling of a complete aircraft configuration ⋮ On the profit of optimizing the fin-keel of a yacht sailing close to wind ⋮ Advances in the linear/nonlinear control of aeroelastic structural systems ⋮ Application of a three-field nonlinear fluid-structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter