The invention provides direct-connection
test equipment for simulating the actual inlet conditions of a
scramjet engine isolation section and
combustion chamber. The direct-connection
test equipment comprises an equipment jet
pipe which is used for accelerating
airflow to the target Mach number, a boundary layer development section which is used for generating a boundary layer, an expansion section which is used for generating accurate oblique
shock wave and an engine isolation section model. The equipment jet
pipe is firstly arranged, the outlet of the equipment jet
pipe is connected with the inlet of the boundary layer development section, the outlet of the boundary layer development section is connected with the inlet of the expansion section, and the outlet of the expansion section is connected with the isolation section model. The
airflow is accelerated to the target Mach number through the equipment jet pipe, a non-uniform boundary layer with inconsistent thickness of the upper and lower wall boundary
layers is formed through the boundary layer development section, and then the
airflow enters the expansion section to generate the accurate oblique
shock wave so that the airflow parameters consistent with the actual inlet conditions of the
scramjet engine isolation section and
combustion chamber can be formed. Meanwhile, a
shock wave generator has an expansion configuration so that the starting problem of the conventional direct-connection
test equipment can be solved.