International Journal of Aerospace Engineering / 2017 / Article / Fig 9

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.