Change in the parameters of a supersonic flow in the presence of transverse blowing

Abstract

A study has been made of the flow formed in a supersonic nozzle when gas is blown in a transverse jet into an expanding supersonic flow. Measurements were made of the total and static pressures of the flow at several sections of the nozzle. It was established that, depending on the relative flow rate α = mj/(mj+ m0) of the blown gas (mjand m0 are the flow rates of the blown gas and the main flow, respectively), there exist two flow regimes with different α dependences of the Mach number of the flow. At small α, the experimental flow parameters correspond satisfactorily to the parameters calculated in a one-dimensional model with a narrow mixing layer near the blowing section. Agreement was observed at flow rates less than a certain α*, this critical value being determined in the model as the flow rate at which the flow after mixing becomes sonic. In the experiments at large flow rates of the blown gas, α* < α < 1, the value of M for the flow hardly depends on α and corresponds to the calculated value of M for a supersonic flow having the velocity of sound near the blowing section. A scheme is proposed for calculating the flow in a nozzle with transverse blowing in the supersonic part; it describes satisfactorily the experimental results in the complete range of blown-gas-main-flow flow rate ratios (0 ≤ α ≤1) over the complete length of the nozzle.