Documentation of Experimental Data for Hypersonic 3-D Shock Waves

Kurzfassung

Experimental data for a series of three-dimensional hypersonic swept- and crossing-shock-waves / turbulent boundary layer interaction flows in the vicinity of one and two sharp fins mounted on a flat plate are presented. The data contains detailed documentation of incoming boundary layer, surface pressure and heat flux distributions, skin friction distributions and topological features of the limiting streamlines in the interaction region at M = 5. The deflection angles ß were varied for swept-shock interactions (single fin geometry) from 0° to 27°, and for crossing-shock interaction (double fin geometry) from 8° to 23°.