Control of the Laminar Separation Bubble on a Plunging Airfoil Using Plasma Actuators
A Pande - 2022 - search.proquest.com
The laminar separation bubble on an X-56A wing section is studied experimentally for static
and heaving/plunging conditions at 𝛼= 12 with 𝑅𝑅𝑅𝑅= 200,000 (𝑈∞= 11 𝑚/𝑠), and …
and heaving/plunging conditions at 𝛼= 12 with 𝑅𝑅𝑅𝑅= 200,000 (𝑈∞= 11 𝑚/𝑠), and …