This thesis numerically investigates the laminar-to-turbulent transition in boundary-layer flows on natural laminar flow airfoils under oscillating inflow conditions. Large-scale …
When a laminar boundary layer is subjected to an adverse pressure gradient, laminar separation bubbles can occur. At low Reynolds numbers, the bubble size can be substantial …
A Gross, HF Fasel - AIAA Journal, 2016 - arc.aiaa.org
The modified NACA 64 3-618 airfoil of the Aeromot 200S Super Ximango motorglider was chosen for wing section simulations at R e= 300,000 and α= 15 deg. A coarse-grid direct …
An investigation of laminar separation bubble behavior on an oscillating X-56A wing section has been performed experimentally at Reynolds number 200,000. Wind tunnel results along …