THE INVISOID FLOW OF REACTING AND RADIANT AIR PAST A HYPERSOMIC BLUNT BODY

摘要

The inviscid hypersonic flow around an arbitrary blunt body of revolution has been formulated for machine computation. The highly accurate stream-tube continuity method was extended to cover the case of chemically reacting and thermally radiating optically thin air, when the flow is in complete thermodynamic and chemical equilibrium.