On a uniformly valid analytical rectilinear cascade response function
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Publication:3075826
DOI10.1017/S0022112010003368zbMath1205.76240MaRDI QIDQ3075826
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Publication date: 17 February 2011
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Related Items (4)
Three-dimensional effects of cascade perforations on rotor–stator interaction noise ⋮ On the flow-acoustic coupling of fan blades with over-the-rotor liner ⋮ The acoustic analogy in an annular duct with swirling mean flow ⋮ An analytic solution for gust–cascade interaction noise including effects of realistic aerofoil geometry
Cites Work
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- The scattering of vorticity waves by an infinite cascade of flat plates in subsonic flow
- Sound Generated by Rotor Wakes Interacting with a Leaned Vane Stator
- The interaction between a high-frequency gust and a blade row
- High frequency thin-airfoil theory for subsonic flow
- Vane Sweep Effects on Rotor/Stator Interaction Noise
- Scattering of incident disturbances by an annular cascade in a swirling flow
- On sound generation by the interaction between turbulence and a cascade of airfoils with non-uniform mean flow
- A uniform asymptotic approximation for high-frequency unsteady cascade flow
- On applications of high-frequency asymptotics in aeroacoustics
- Sound generation by turbulence and surfaces in arbitrary motion
- Sound transmission through blade
- Generation of sound by rotor-stator interaction
- Similarity rules for thin aerofoils in non-stationary subsonic flows
- On the transmission of sound waves through a blade row
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