Numerical and Experimental Study on the Duration of Nozzle Starting of the Reflected High-Enthalpy Shock Tunnel

Abstract

The starting process of the flow in the nozzle of the JF-14 shock tunnel (1.6 m in length, 500 mm in outlet diameter) in the State Key Laboratory of High Temperature Gas Dynamics is analyzed by calculation and experiment. Two key factors which directly affect the duration of the nozzle starting are the velocity of the expansion wave and the low-velocity zone generated by the interaction between the secondary shock wave and boundary layer on the wall surface. In the process of the nozzle starting, the flow field stabilizes at the center of the nozzle outlet first, and then gradually stabilizes along the radius direction, thus defining the central startup and complete startup of the nozzle. It is found that there is a critical initial pressure. When the initial pressure is lower than the critical pressure, the airflow can reach stability in the nozzle outlet center with the shortest time, otherwise, the time required is much longer. The time required for the airflow to stabilize in the whole outlet section is mainly affected by the size of the low-velocity zone. It is also found that only at a very low initial pressure can the airflow simultaneously reach stability at the entire outlet of the nozzle.

Investigation of Shock Wave Oscillation Suppression by Overflow in the Supersonic Inlet

“…The shock/boundary layer interaction is an important flow phenomenon in supersonic and hypersonic inlets [1], which also generally exists in supersonic pipeline flows [2], such as the nozzle flow [3]. When the combustor backpressure becomes higher, the backpressure shock moves forward, and the shock evolves into a complex shock train system [4][5][6], so an equal cross-sectional area isolator is usually set to hold the shock train [7,8].…”