The invention discloses an exhaust apparatus for an exhaust
simulation test of an exhaust
nozzle of a supersonic engine. The exhaust apparatus comprises a
tail chamber and an ejector, the
tail chamber comprises a fixed large
tail chamber and a replaceable small tail chamber, the fixed large tail chamber comprises a tail chamber convergence segment, a tail chamber equal-
diameter segment, and a tail chamber expansion segment, the replaceable small tail chamber comprises a small tail chamber
flange and a small tail chamber cylinder body, the small tail chamber cylinder body is arranged in the tail chamber convergence segment, the fixed large tail chamber is provided with a circulating cooling water device and a cooling water spraying device, the ejector comprises a low-pressure chamber, a transition segment, a blending convergence segment, a blending equal-
diameter segment and a blending expansion segment, the inner part of the low-pressure chamber is fixedly connected with a circular ring diversion and guiding device, an ejection
airflow conveying pipeline, an ejection
airflow convergence segment and an ejection
airflow expansion segment, and cross sections of an outlet of the low-pressure chamber and an outlet of the ejection airflow expansion segment are located in the same
vertical plane. According to the exhaust apparatus,
test requirements for simulating high-altitude flight states of different supersonic engines on the ground can be met.