The nonuniform temperature distribution (NUTD) on the coherent vortex surfaces of hypersonic turbulent boundary layer (TBL) is studied using the conditional sampling technique. The direct numerical simulation data of Mach 8 flat-plate TBL flows with different wall temperatures, T-w/T-infinity = 10.03 and 1.9, are used for this research, and the coherent vortex surface is identified by the O-criterion. Two characteristic sides of the vortex are defined, which are represented by the positive and negative streamwise velocity fluctuations (+/- u') of the vortex surfaces. The conditional sampling results between the mean temperature of the two sides show that there is a significant difference of up to 20% at the same wall-normal location. Furthe...
Direct numerical simulations (DNS) of Mach 6 turbulent boundary layer with nominal freestream Mach n...
Measurements of both the velocity and the temperature field have been made in the thermal layer that...
Measurements of both the velocity and the temperature field have been made in the thermal layer that...
The nonuniform temperature distribution (NUTD) on the coherent vortex surfaces of hypersonic turbule...
The nonuniform temperature distribution (NUTD) on the coherent vortex surfaces of hypersonic turbule...
The correlation between density and temperature fluctuations (rho ' and T ') of the turbulent bounda...
Coherent structures near the wall (y^+<60)in a turbulent channel flow were educed by a conditional s...
This paper reports the direct numerical simulation (DNS) for hypersonic turbulent boundary layer ove...
International audienceThe present work is dedicated to the numerical study of statistical characteri...
International audienceThe present work is dedicated to the numerical study of statistical characteri...
International audienceThe present work is dedicated to the numerical study of statistical characteri...
High-speed vehicles experience a highly challenging environment in which the freestream Mach number ...
This work investigates the non-uniform total temperature and total pressure downstream of a circular...
This work investigates the non-uniform total temperature and total pressure downstream of a circular...
This work investigates the non-uniform total temperature and total pressure downstream of a circular...
Direct numerical simulations (DNS) of Mach 6 turbulent boundary layer with nominal freestream Mach n...
Measurements of both the velocity and the temperature field have been made in the thermal layer that...
Measurements of both the velocity and the temperature field have been made in the thermal layer that...
The nonuniform temperature distribution (NUTD) on the coherent vortex surfaces of hypersonic turbule...
The nonuniform temperature distribution (NUTD) on the coherent vortex surfaces of hypersonic turbule...
The correlation between density and temperature fluctuations (rho ' and T ') of the turbulent bounda...
Coherent structures near the wall (y^+<60)in a turbulent channel flow were educed by a conditional s...
This paper reports the direct numerical simulation (DNS) for hypersonic turbulent boundary layer ove...
International audienceThe present work is dedicated to the numerical study of statistical characteri...
International audienceThe present work is dedicated to the numerical study of statistical characteri...
International audienceThe present work is dedicated to the numerical study of statistical characteri...
High-speed vehicles experience a highly challenging environment in which the freestream Mach number ...
This work investigates the non-uniform total temperature and total pressure downstream of a circular...
This work investigates the non-uniform total temperature and total pressure downstream of a circular...
This work investigates the non-uniform total temperature and total pressure downstream of a circular...
Direct numerical simulations (DNS) of Mach 6 turbulent boundary layer with nominal freestream Mach n...
Measurements of both the velocity and the temperature field have been made in the thermal layer that...
Measurements of both the velocity and the temperature field have been made in the thermal layer that...