Sound generation by a supersonic aerofoil cutting through a steady jet flow
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Publication:3476479
DOI10.1017/S0022112090000398zbMath0698.76068MaRDI QIDQ3476479
No author found.
Publication date: 1990
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Related Items (4)
The viscous interaction between sound waves and the trailing edge of a supersonic splitter plate ⋮ Asymptotic analysis of the radiation by volume sources in supersonic rotor acoustics ⋮ Canonical sound fields in the frequency-domain theory of supersonic leading-edge noise ⋮ Basic singular fields in the theory of impulsive supersonic leading-edge noise
Cites Work
- Sound generated from the interruption of a steady flow by a supersonically moving aerofoil
- The dissipation of sound at an edge
- Acoustics as a branch of fluid mechanics
- Sound diffraction at a trailing edge
- Low-frequency sound radiation and generation due to the interaction of unsteady flow with a jet pipe
- The influence of vortex shedding on the generation of sound by convected turbulence
- Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half plane
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