SINGLE-COMPONENT MOLECULAR TAGGING VELOCIMETRY OF THE BOUNDARY LAYER ON A NACA-0012 AIRFOIL PLUNGING ACROSS UNIFORM-SHEAR FLOW

von Albrecht, Mitchell B.
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Fluid dynamics ; Volume 7 of 7 (2020)

Reynolds Number and Freestream Shear Effects on a NACA 0012 Airfoil in the Reynolds Number Range 10,000-30,000

von Albrecht, Mitchell B.
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Fluid dynamics ; Volume 2 of 7 (2022)