The present invention relates to the field of wind tunnel testing, and provides an ejector slot follow-up adjustment mechanism, a flow field control method and
system, the mechanism comprising an ejector slot formed by a test section air-permeable wall panel and a test section
solid wall panel located on both sides of the flow field, and a rotation center and a scimitar mechanism located in the middle of the flow field; and also comprising a
servo motion mechanism, which is respectively connected to the test section
solid wall panels on both sides of the flow field, and is used to drive the test section
solid wall panels to control the opening of the ejector slot. During the test, the ejector slot opening on both sides of the flow field is adjusted according to the sideslip angle formed by the deflection of the scimitar mechanism. The present invention proposes a driving mechanism that can realize the continuous movement of the sideslip angle of the model, and the movement of the sideslip angle is completely decoupled from the movement of the
angle of attack and does not affect each other; by introducing a
servo motion mechanism to dynamically adjust the ejector slot opening according to the sideslip angle, the difference in the flow area on both sides of the scimitar mechanism can be minimized as much as possible, thereby reducing the
asymmetry of the left and right flow fields, reducing the
lateral deviation angle of the
airflow, and better reducing the interference of the bracket.