Research Article
Experimental Study on Aerodynamic Heating Induced by Dual Injections into Hypersonic Cross Flow
Figure 9
Stanton number profile on -axis obtained by TSP, thermocouples, and Lees’ equation (as a reference) under no-injection condition at ms. The upper and lower broken lines indicate the range of uncertainty of the TSP measurements. The error bar of thermocouple data indicates ±1σ calculated with data obtained in two runs.