Published January 1, 1992 | Version v1
Report

A numerical study of inviscid, supersonic mixing layers

  • 1. Univ. of Washington, Seattle (United States)

Description

The purpose of this research is to understand the physical processes associated with turbulent mixing in supersonic shear layers. Specifically, the evolution of instabilities in two and three-dimensional, confined and unconfined, temporal shear layers are studied. Both linear stability theory and direct numerical simulation are used. For the two-dimensional, supersonic, confined layer, two distinct modes of instability are found, a symmetric and an asymmetric mode. In both cases the instability grows nonlinearly with large amplitude disturbances that never roll up like the classical Kelvin-Helmholtz instability. Another mode of instability is found for the confined, transonic layer where a higher mode is excited from a nonlinear interaction of the walls with the fundamental mode. The most unstable modes for the three-dimensional layer at supersonic relative Mach numbers is purely three-dimensional, i.e. oblique to the flow direction

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. 183-192.
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
24064068
Subject category
S42: ENGINEERING;
Resource subtype / Literary indicator
Conference
Descriptors DEI
COMBUSTION; IDEAL FLOW; INSTABILITY; LAYERS; MACH NUMBER; MIXING; NUMERICAL SOLUTION; SHEAR; SUPERSONIC FLOW; TWO-DIMENSIONAL CALCULATIONS
Descriptors DEC
CHEMICAL REACTIONS; FLUID FLOW; INCOMPRESSIBLE FLOW; OXIDATION; STEADY FLOW; VELOCITY

Optional Information

Contract/Grant/Project number
Contract N00014-87-K-0174