The influence of turbulence inflow generation on direct numerical simulations (DNS) of high-speed turbulent boundary layers at Mach numbers of 2 and 5.84 is investigated. Two main classes of inflow conditions are considered, based on the recycling/rescaling (RR) and the digital filtering (DF) approach, along with suitably modified versions. A series of DNS using very long streamwise domains is first carried out to provide reliable data for the subsequent investigation. A set of diagnostic parameters is then selected to verify achievement of an equilibrium state, and correlation laws for those quantities are obtained based on benchmark cases. Simulations using shorter domains, with extent comparable with that used in the current literature, ...
This paper reports the direct numerical simulation (DNS) for hypersonic turbulent boundary layer ove...
Although the Radiatively Driven Hypersonic Wind-Tunnel concept overcomes the need for very high rese...
Thesis (Master's)--University of Washington, 2013In flight vehicles, a large portion of fuel consump...
Direct numerical simulations (DNS) of hypersonic turbulent boundary layers and their freestream acou...
This paper presents a direct numerical simulation database of high-speed zero-pressure-gradient turb...
We study the organization of turbulence in supersonic boundary layers through large-scale direct num...
Nearly all moving objects on Earth pass through fluids and many of them move at high speed. This mak...
We study the structure of high-speed zero-pressure-gradient turbulent boundary layers up to friction...
We present a direct numerical simulation database of supersonic and hypersonic turbulent boundary la...
We study the high-Reynolds-number behavior of a turbulent boundary layer in the low supersonic regim...
The effects of surface roughness on compressible turbulent flow have not been studied as closely as ...
Direct numerical simulations (DNSs) of a turbulent boundary layer (TBL) with Re??=570-2560 were perf...
A new high-resolution code for the direct numerical simulation of a zero pressure gradient turbulent...
A direct numerical approach has been developed to simulate supersonic turbulent boundary layers. The...
Direct Numerical Simulations are used to generate a database of high-speed zero-pressure-gradient tu...
This paper reports the direct numerical simulation (DNS) for hypersonic turbulent boundary layer ove...
Although the Radiatively Driven Hypersonic Wind-Tunnel concept overcomes the need for very high rese...
Thesis (Master's)--University of Washington, 2013In flight vehicles, a large portion of fuel consump...
Direct numerical simulations (DNS) of hypersonic turbulent boundary layers and their freestream acou...
This paper presents a direct numerical simulation database of high-speed zero-pressure-gradient turb...
We study the organization of turbulence in supersonic boundary layers through large-scale direct num...
Nearly all moving objects on Earth pass through fluids and many of them move at high speed. This mak...
We study the structure of high-speed zero-pressure-gradient turbulent boundary layers up to friction...
We present a direct numerical simulation database of supersonic and hypersonic turbulent boundary la...
We study the high-Reynolds-number behavior of a turbulent boundary layer in the low supersonic regim...
The effects of surface roughness on compressible turbulent flow have not been studied as closely as ...
Direct numerical simulations (DNSs) of a turbulent boundary layer (TBL) with Re??=570-2560 were perf...
A new high-resolution code for the direct numerical simulation of a zero pressure gradient turbulent...
A direct numerical approach has been developed to simulate supersonic turbulent boundary layers. The...
Direct Numerical Simulations are used to generate a database of high-speed zero-pressure-gradient tu...
This paper reports the direct numerical simulation (DNS) for hypersonic turbulent boundary layer ove...
Although the Radiatively Driven Hypersonic Wind-Tunnel concept overcomes the need for very high rese...
Thesis (Master's)--University of Washington, 2013In flight vehicles, a large portion of fuel consump...