Numerical Solution of the Steady Laminar Hypersonic Boundary Layer Equations at Chemical Nonequilibrium,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
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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.
- Fluid Mechanics