Linearized analysis of the three-dimensional compressible flow through a rotating annular blade row

DOI10.1017/S0022112081001407zbMath0483.76084OpenAlexW2047869056MaRDI QIDQ3942639

John A. Lordi, Gregory F. Homicz

Publication date: 1981

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

Full work available at URL: https://doi.org/10.1017/s0022112081001407

zbMATH Keywords

three-dimensionalstrip theorylinearized solutionlifting surfaceannular rotating blade row within long ductcoordinate system attached to blademass-source solutionpressure-dipole solutionrotor- loading conditionsmall disturbance fieldthickness-induced camberline configurationvortex representation

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Related Items (3)

Three-dimensional effects of cascade perforations on rotor–stator interaction noise ⋮ On the flow-acoustic coupling of fan blades with over-the-rotor liner ⋮ On the use of the method of matched asymptotic expansions in propeller aerodynamics and acoustics

Cites Work

• Three-dimensional analysis of blade force and sound generation for an annular cascade in distorted flows

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