Simulation and modeling of homogeneous, compressed turbulence
Description
Low Reynolds number homogeneous turbulence undergoing low Mach number isotropic and one-dimensional compression was simulated by numerically solving the Navier-Stokes equations. The numerical simulations were performed on a CYBER 205 computer using a 64 x 64 x 64 mesh. A spectral method was used for spatial differencing and the second-order Runge-Kutta method for time advancement. A variety of statistical information was extracted from the computed flow fields. These include three-dimensional energy and dissipation spectra, two-point velocity correlations, one-dimensional energy spectra, turbulent kinetic energy and its dissipation rate, integral length scales, Taylor microscales, and Kolmogorov length scale. Results from the simulated flow fields were used to test one-point closure, two-equation models. A new one-point-closure, three-equation turbulence model which accounts for the effect of compression is proposed. The new model accurately calculates four types of flows (isotropic decay, isotropic compression, one-dimensional compression, and axisymmetric expansion flows) for a wide range of strain rates
Availability note (English)
Available from NTIS, PC A10/MF A01.Additional details
Publishing Information
- Imprint Pagination
- 206 p.
- Report number
- N--86-30958
INIS
- Country of Publication
- United States
- Country of Input or Organization
- United States
- INIS RN
- 18023201
- Subject category
- S42: ENGINEERING;
- Resource subtype / Literary indicator
- Numerical Data, Non-conventional Literature
- Descriptors DEI
- COMPRESSIBLE FLOW; COMPUTERIZED SIMULATION; ENERGY SPECTRA; KINETIC ENERGY; MOTORS; NAVIER-STOKES EQUATIONS; NUMERICAL SOLUTION; STRAIN RATE; THEORETICAL DATA; TURBULENT FLOW
- Descriptors DEC
- DATA; DIFFERENTIAL EQUATIONS; ENERGY; EQUATIONS; FLUID FLOW; INFORMATION; NUMERICAL DATA; PARTIAL DIFFERENTIAL EQUATIONS; SIMULATION; SPECTRA
Optional Information
- Secondary number(s)
- NASA-CR--176939; NAS--1.26:176939; SU-TF--21.