supersonic boundary layeraero-optical effectwall temperaturewall blowing and suctionAero-optical reduction in flat-plate turbulent boundary layer has been widely concerned due to critical application for high-speed target-seeking vehicles. From the perspective of disciplinary intersection between aerodynamic ...
He Lin,Yi Shi-He,Tian Li-Feng,Chen Zhi,Zhu Yang-Zhu.Simultaneous density and velocity measurements in a supersonic turbulent boundary layer[J]. Chinese Physics B .2013(2)Simultaneous density and velocity measurements in a supersonic turbulent boundary layer. Lin He,Shi-He Yi,Li-Feng Tian,...
Wide-field particle image velocimetry measurements were performed in a Mach 2 turbulent boundary layer to study the characteristics of large-scale coherence at two wall-normal locations (gamma/delta=0.16 and 0.45). Instantaneous velocity fields at both locations indicate the presence of elongated stream...
An investigation has been made into the effect of a step change in wall temperature on a turbulent boundary layer in a supersonic flow at a Mach number of 2.3. Measurements of the mean and turbulent flowfields were made. The results show that the relaxation behavior in general is slow excep...
A spatially developing supersonic turbulent boundary layer at a Mach number of 2.5 and Reynolds numbers 2287 ≤ % MathType!MTEF!2!1!+- % feaagCart1ev2aqatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn % hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr % 4rNCHbWexLMBbXgBd9gzLbvyNv2Cae...
Schreyer A M,Gaisbauer U,Kr?mer E. Seventh IUTAM Symposium on Laminar-Turbulent Transition . 2010A. M. Schreyer, U. Gaisbauer, and E. Kramer, "Fluctuation measure- ments in the turbulent boundary layer of a supersonic flow," Pamm, vol. 18, pp. 569-572, 2010....
Large-eddy simulation of a supersonic turbulent boundary layer over a compression-expansion ramp Int J Heat Fluid Fl (2013) P.L.Ardonceau The structure of turbulence in a supersonic shock wave/ boundary layer interaction AIAA J (1984) ...
Measurement of mean flow profiles in a fully developed Mach 3 turbulent boundary layer with negligible pressure gradient is reported. Data were acquired at several streamwise locations for wall-to-total temperature ratios of 0.94, 0.71, and 0.54. The results demonstrate that the velocity defect formu...
An experimental study is made of the turbulent boundary layer in its interaction with a shock wave, the purpose being to clarify questions connected with the increase in the fullness of the velocity profiles. New systematic data are obtained on the development of the boundary layer, and its stru...
Laminar-turbulent transition of supersonic boundary layer in the presence of external disturbances. Thermophys. Aeromech. 26, 375–383 (2019). https://doi.org/10.1134/S0869864319030065 Download citation Received16 November 2018 Revised28 December 2018 Accepted28 February 2019 Published28 August 2019 ...