Laminar Heat Exchange on Sharp and Blunt Plates in a Hypersonic Air Flow

摘要

The results of an experimental investigation and numerical simulation of heat exchange are given for sharp and blunt plates in a hypersonic air flow. The experiments were carried out in a Ludwig-type wind tunnel at hypersonic Mach numbers and a Reynolds number Re{sub}L which varied over the range from 0.24 · 10{sup}6 to 1.31 · 10{sup}6. The bluntness radius r was varied over the range from 0.008 mm (almost sharp plate) to 4 mm (the corresponding Reynolds numbers Re{sub}r from 15 to 4 · 10{sup}4). The numerical simulation was carried out by solving the complete two-dimensional Navier-Stokes equations. The experimental data were correlated using the well-known viscous hypersonic interaction parameters.