Supersonic turbulent boundary layer drag control using spanwise wall oscillation

Physics & Astronomy

• supersonic boundary layers 100%
• drag reduction 87%
• turbulent boundary layer 73%
• drag 64%
• oscillations 42%
• alternating current 20%
• Reynolds number 14%
• Mach number 11%
• trends 8%
• compressible flow 7%
• incompressible flow 7%
• channel flow 6%
• direct numerical simulation 5%
• spacing 4%
• scaling 3%

Engineering & Materials Science

• Drag reduction 82%
• Boundary layers 63%
• Drag 61%
• Reynolds number 14%
• Mach number 11%
• Direct numerical simulation 7%
• Compressible flow 7%
• Incompressible flow 6%
• Channel flow 6%