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
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