Publication Date:
2019-07-13
Description:
The three-dimensional time dependent equations of motion were numerically integrated for fully-developed turbulent channel flow. A large scale flow field was obtained directly from the solution of these equations, and small scale field motions were simulated through an eddy viscosity model. The calculations were carried out on the ILLIAC 4 computer. The computed flow patterns show that the wall layer consists of coherent structures of low speed and high speed streaks alternating in the spanwise direction. These structures were absent in the regions away from the wall. Hot spots, small localized regions of very large turbulent shear stress, were frequently observed. The profiles of the pressure velocity-gradient correlations show a significant transfer of energy from the normal to the spanwise component of turbulent kinetic energy in the immediate neighborhood of the wall ('the splatting effect').
Keywords:
AERONAUTICS (GENERAL)
Type:
NASA-TM-78619
,
A-7952
,
AGARD Symp. on Turbulent Boundary Layer, Experiment, Theory, and Modelling; Sep 24, 1979 - Sep 27, 1979; The Hague; Netherlands
Format:
application/pdf
