In this paper a study is presented of the separated flow properties and corresponding aerodynamic behaviors of a high-AOA, NACA 633-018 airfoil under internal acoustically pulsing excitation in a subsonic wind tunnel. The measurements by means of pitot-static pressure tube and hot-wire anemometer in
A Geometrical Acoustics Approach for Calculating the Effects of Flow on Acoustics Scattering
β Scribed by N. Atalla; S. Glegg
- Publisher
- Elsevier Science
- Year
- 1994
- Tongue
- English
- Weight
- 446 KB
- Volume
- 171
- Category
- Article
- ISSN
- 0022-460X
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β¦ Synopsis
A ray acoustics approach to flow effects on acoustics scattering is considered, based on a combination of geometrical acoustics and the paraxial ray approximation. The approach allows for scattering by objects of arbitrary shapes, inhomogeneous and moving media. Applications to flow effects on scattering include the effect of a wall shear layer on scattering from a cylindrical shaped fuselage and the effects of an incompressible inviscid flow on the directivity pattern of the scattered field from a cylinder and a Rankine body. It has been found that the flow causes a modification and displacement of the lobes of the directivity pattern and the shadow zone of the scattered field, which can be important at Mach numbers greater than (0 \cdot 2).
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