This paper concerns the calculation of the sound fields which are generated when a vortical gust, convected in a supersonic mean flow, strikes the leading edge of a fan blade or aerofoil. Inviscid linear theory is applied, with the blade modelled as an infinite-span flat rigid plate, and a gust of a
β¦ LIBER β¦
A generalized theory on the noise generation from supersonic shear layers
β Scribed by S.P. Pao
- Publisher
- Elsevier Science
- Year
- 1971
- Tongue
- English
- Weight
- 815 KB
- Volume
- 19
- Category
- Article
- ISSN
- 0022-460X
No coin nor oath required. For personal study only.
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