On the use of the method of matched asymptotic expansions in propeller aerodynamics and acoustics

DOI10.1017/S0022112092002301zbMath0755.76092MaRDI QIDQ4020292

H. H. Brouwer

Publication date: 16 January 1993

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

zbMATH Keywords

integral equationdownwash velocityuniform axial flowPrandtl's lifting line equation

Mathematics Subject Classification ID

General theory of rotating fluids (76U05) Asymptotic expansions of solutions to PDEs (35C20) Hydro- and aero-acoustics (76Q05)

Cites Work

• Unsteady lifting-line theory by the method of matched asymptotic expansions
• Linearized analysis of the three-dimensional compressible flow through a rotating annular blade row
• Some notes on unsteady lifting-line theory
• The importance of quadrupole sources in prediction of transonic tip speed propeller noise
• Lifting-line theory as a singular-perturbation problem

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