Hyposonic aerodynamics (flows at low mach numbers)
β Scribed by R. Kh. Zeitunyan
- Book ID
- 105001553
- Publisher
- SP MAIK Nauka/Interperiodica
- Year
- 1984
- Tongue
- English
- Weight
- 725 KB
- Volume
- 24
- Category
- Article
- ISSN
- 0021-8944
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
A review is made of the di!raction theory of the trailing edge noise generated by a #at-plate airfoil of zero-thickness and non-compact chord, according to which the sound is attributed to the scattering of a &&frozen'' pattern of turbulence wall pressure swept over the edge in the mean #ow. Extensi
## Abstract The latticeβBGK method has been extended by introducing additional, free parameters in the original formulation of the latticeβBGK methods. The relationship between these parameters and the macroscopic moment equations is analysed by Taylor series and ChapmanβEnskog expansion. The param
The di!raction theory of Part 1 [1] for estimating the sound generated by low Mach number #ow past the trailing edge of an airfoil of compact, but "nite thickness is applied to investigate the noise produced by turbulent #ow over an edge whose upper surface pro"le (the suction side) is rounded. The