๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Large-eddy simulation of transitional channel flow

โœ Scribed by Ugo Piomelli; Thomas A. Zang


Publisher
Elsevier Science
Year
1991
Tongue
English
Weight
445 KB
Volume
65
Category
Article
ISSN
0010-4655

No coin nor oath required. For personal study only.

โœฆ Synopsis


A large-eddy simulation (LES) of transition in plane channel flow has been carried out. The LES results have been compared with those of a fine direct numerical simulation (DNS), and with those of a coarse DNS that uses the same mesh as the LES, but no residual stress model. While at the early stages of transition LES and coarse DNS give the same results, the presence of the residual stress model was found to be necessary to predict accurately mean velocity and Reynolds stress profiles during the late stages of transition (after the second spike stage). The evolution of single Fourier modes is also predicted more accurately by the LES than by the coarse DNS. As small scales are generated, the dissipative character of the residual stress causes it to reproduce correctly the energy cascade; as transition progresses, then, and the flow approaches its fully developed turbulent state, the subgrid scales tend towards equilibrium and the model becomes more accurate.


๐Ÿ“œ SIMILAR VOLUMES


Large eddy simulation in a turbulent cha
โœ T. Cziesla; G. Biswas; N.K. Mitra ๐Ÿ“‚ Article ๐Ÿ“… 1999 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 164 KB ๐Ÿ‘ 2 views

The influence of the exit boundary conditions on the vanishing first derivative of the velocity components and constant pressure on the large eddy simulation of the fully developed turbulent channel flow has been investigated for equidistant and stretched grids at the channel exit. Results show that

Large eddy simulation of subsonic and su
โœ E. Lenormand; P. Sagaut; L. Ta Phuoc ๐Ÿ“‚ Article ๐Ÿ“… 2000 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 327 KB ๐Ÿ‘ 1 views

Large eddy simulation (LES) of compressible periodic channel flow is performed using a fourth-order finite difference scheme for a Reynolds number based on bulk density, bulk velocity and channel half-width equal to 3000. Two configurations are studied: a subsonic case (M 0 = 0.5) that corresponds t