Published January 1, 1992 | Version v1
Report

Shock enhancement of a turbulent flow

Creators

  • 1. Lawrence Livermore National Lab., CA (United States)

Description

Presented here are calculations describing the enhancement of turbulence caused by the passing of a shock wave. This field is of interest to those investigating the Richtmyer-Meshkov instability, supersonic combustion, fusion and many others. Experiments involving shocks and turbulence (Sturtevant, et. al. 1980, Smits and Muck 1987, Trolier and Duffy 1984) show that the turbulence level following a shock wave can be as much as 3 times higher then that before the shock. Predictions from linear theory (McKenzie and Westphal 1968 and Anyiwo and Bushnell 1982) show very similar shock enhancements. Recent calculations involving nonlinear effects (Kumar et. al. 1987 and Viecelli 1988) show promise in explaining how this enhancement is obtained. This study will use a shock tube type calculation domain to investigate the effect of a shock wave on pre-existing turbulence

Part of:
Advances in compressible turbulent mixing

Additional details

Publishing Information

Imprint Title
Advances in compressible turbulent mixing
Imprint Pagination
634 p.
Journal Page Range
p. 553-562.
Report number
CONF-8810234--

Conference

Title
Workshop on the physics of compressible turbulent mixing.
Dates
24-27 Oct 1988.
Place
Princeton, NJ (United States).

INIS

Country of Publication
United States
Country of Input or Organization
United States
INIS RN
24064101
Subject category
S42: ENGINEERING;
Resource subtype / Literary indicator
Conference
Descriptors DEI
GAS FLOW; MIXING; NUMERICAL SOLUTION; SHEAR; SHOCK WAVES; SUPERSONIC FLOW; TURBULENCE; TURBULENT FLOW; VORTICES
Descriptors DEC
FLUID FLOW

Optional Information