Two-dimensional viscous flow computations of hypersonic scramjet nozzle flowfields at design and off-design conditions

摘要

The PARC2D code has been selected to analyze the flowfields of a representative hypersonic scramjet nozzle over a range of flight conditions from Mach 3 to 20. The flowfields, wall pressures, wall skin friction values, heat transfer values and overall nozzle performance are presented.