COMPUTER PROGRAMS FOR A REACTIVE TURBULENT BOUNDARY LAYER AIR VERSION
Abstract
Computer programs for the calculation of properties within a reactive compressible turbulent air boundary layer on a flat plate are described. The pressure is constant throughout the boundary layer. The partial differential equations for energy and species mass conservation are solved with arbitrary initial conditions by a finite difference technique. A variable wall temperature boundary condition may be used. The boundary conditions at the edge of the boundary layer are constant with respect to the axial coordinate. The partial differential equations, which describe a two-dimensional diffusing flow, may be coupled to a system of equations describing a one-dimensional finite-rate air chemically reacting flow, and hence may be used in the numerical treatment of the two-dimensional reacting boundary layer.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 15, 1965
- Accession Number
- AD0627474
Entities
People
- B. Bellow