Numerical Solution of the Steady Laminar Hypersonic Boundary Layer Equations at Chemical Nonequilibrium,
Abstract
An implicit finite difference method is presented for the numerical solution of the steady laminar two-dimensional hypersonic boundary layer equations at chemical nonequilibrium. The strong nonlinearity of the energy equation and of the continuity equations due to the influence of chemical reactions requires a combination of the Newton iteration method and the method of finite differences.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 25, 1975
- Accession Number
- ADA017197
Entities
People
- D. Straub
- E. Adams
- H. Spreuer
- W. Schonauer
Organizations
- National Air and Space Intelligence Center