Subsonic flow past thick wing in ground effect, lifting line theory
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Publication:753578
DOI10.1007/BF01173739zbMath0716.76045MaRDI QIDQ753578
Publication date: 1990
Published in: Acta Mechanica (Search for Journal in Brave)
General aerodynamics and subsonic flows (76G25) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)
Related Items (2)
A numerical solution for the equation of the lifting surface in ground effects ⋮ Generalized Weissinger's L-method for prediction of curved wings operating above a free surface in subsonic flow
Cites Work
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- Method of fundamental solutions in plane steady linear aerodynamics
- The theory of oscillating thick wings in subsonic flow. Lifting line theory
- Thickness and camber effects in slender wing theory
- Analysis of small-aspect-ratio lifting surfaces in ground effect
- Stationary Fundamental Solution for an Ideal Fluid in Uniform Motion
- An analytic solution for two- and three-dimensional wings in ground effect
- Note on the Theory of Lifting Surfaces
- Nonaxisymmetric compressible swirling flow in turbomachine annuli
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