Accession Number:

ADA017197

Title:

Numerical Solution of the Steady Laminar Hypersonic Boundary Layer Equations at Chemical Nonequilibrium,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1975-06-25

Pagination or Media Count:

80.0

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.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE