Aerodynamic characteristics of pretensioned elastic membrane rectangular sailwings

DOI10.1016/0045-7825(84)90117-8zbMath0525.73057OpenAlexW2079178964MaRDI QIDQ593845

Sumit K. Garg

Publication date: 1984

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7825(84)90117-8

zbMATH Keywords

iterative procedureaerodynamic characteristicsnonlinear problemadmissible mode shape for inflated elastic saildoublet lattice methodinflated configurationnylon-cotton sailwingpretensioned elastic membrane rectangular sailwingsresults tend to plane wing values when pretensions large in magnitude

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10)

Cites Work

• The aerodynamic theory of sails. I. Two-dimensional sails
• Theory of Flexible Aerodynamic Surfaces
• A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.

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