Wind-tunnel data on the effect of small-scale stationary flow perturbation on laminar boundary-layer separation in the aft part of a body of revolution are presented. The experimental results obtained at low subsonic velocities through hot-wire measurements support an idea of controlling axisymmetric flow separation locally as it was found earlier in plane configurations on airfoils and wings.
Perturbed laminar flow separating from an axisymmetric body
INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2020) ; 2020 ; Novosibirsk, Russia
AIP Conference Proceedings ; 2351 , 1
24.05.2021
4 pages
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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