Computation of chemically reacting flows
Abstract
A program system was developed to compute twodimensional chemically reacting free jet flow. A calculation mesh which is invariant in time is introduced. The flow equations are transformed by the lambda scheme into the mesh for integration. The shock wave is treated by the shockfitting method. The boundary conditions are taken into account by the post correction method. Velocity, pressure, temperature, and entropy distributions of the reacting mixture components in the flow field are calculated.
 Publication:

In its Thermodyn. and Flow Mech. Problems in Aircraft and Spacecraft Devices: Summary of Work and Results for 1980
 Pub Date:
 1982
 Bibcode:
 1982tfmp.nasa..379A
 Keywords:

 Chemical Reactions;
 Computer Programs;
 Flow Equations;
 Numerical Analysis;
 Entropy;
 Free Jets;
 Pressure Distribution;
 Temperature Distribution;
 Two Dimensional Flow;
 Unsteady Flow;
 Velocity Distribution;
 Fluid Mechanics and Heat Transfer