A discussion is given of the production of sound by low Mach number turbulent flow over the trailing edge of a serrated airfoil. The airfoil is modeled by a fiat plate set at zero angle of attack to the mean flow, and attention is given to both limiting cases in which the chord of the airfoil is eit
β¦ LIBER β¦
The displacement-thickness theory of trailing edge noise
β Scribed by M.S. Howe
- Book ID
- 103250633
- Publisher
- Elsevier Science
- Year
- 1981
- Tongue
- English
- Weight
- 916 KB
- Volume
- 75
- Category
- Article
- ISSN
- 0022-460X
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