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February 1976 Part
Turbulent Boundary Layer with Pressure Y Tsuji
Large Deflection of Axisymmetrically
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adverse pressure gradient aerodynamic Aeronautical Quarterly amplitude approximate attachment lines axisymmetric body bubble buckling calculated cent circular cylinder compression cone constant corresponding curve damping deflection delta wing diameter downstream drag coefficient effect equation experimental Fluid Mechanics free-stream turbulence given golf ball hot-wire incidence increase jet-mainstream contour Journal of Fluid leading edge leading-edge separation leeward cylinder lift coefficient lift force load Mach number maximum mean velocity measured method momentum non-dimensional nozzle obtained oscillating outer parameter predicted present pressure distributions pressure gradient range ratio Reference region Reynolds number Reynolds stress Royal Aeronautical Society shear layer shedding frequency shock wave shown in Figure skin friction solution speed spin stagnation pressure static pressure supersonic surface heat exchanger swirling flows thickness thin-shock-layer theory transverse tunnel turbulence levels turbulent boundary layer two-dimensional values velocity profile vortex shedding vortices wake centre line wall yaw angle