In this work, numerical studies are conducted for a supersonic M = 2.0 steady flow over a flat plate with a suction through single circular hole of variating intensity. The computed flow fields near the suction hole are estimated to build special boundary condition of Dirichlet type. Such a simulated suction can be used in DNS of disturbances propagation over walls with multiple suction holes.
Modelling of suction for supersonic laminar flow control
INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2020) ; 2020 ; Novosibirsk, Russia
AIP Conference Proceedings ; 2351 , 1
2021-05-24
11 pages
Conference paper
Electronic Resource
English
Experimental Investigation of Laminar Flow Control on a Supersonic Swept Wing by Suction
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