Verification and validation in computational fluid dynamics
WL Oberkampf, TG Trucano - Progress in aerospace sciences, 2002 - Elsevier
Verification and validation (V&V) are the primary means to assess accuracy and reliability in
computational simulations. This paper presents an extensive review of the literature in V&V …
computational simulations. This paper presents an extensive review of the literature in V&V …
Review and assessment of turbulence models for hypersonic flows
CJ Roy, FG Blottner - Progress in aerospace sciences, 2006 - Elsevier
Accurate aerodynamic prediction is critical for the design and optimization of hypersonic
vehicles. Turbulence modeling remains a major source of uncertainty in the computational …
vehicles. Turbulence modeling remains a major source of uncertainty in the computational …
[图书][B] Turbulent shear layers in supersonic flow
AJ Smits, JP Dussauge - 2006 - books.google.com
A good understanding of turbulent compressible flows is essential to the design and
operation of high-speed vehicles. Such flows occur, for example, in the external flow over …
operation of high-speed vehicles. Such flows occur, for example, in the external flow over …
A numerical study of turbulent supersonic isothermal-wall channel flow
A study of compressible supersonic turbulent flow in a plane channel with isothermal walls
has been performed using direct numerical simulation. Mach numbers, based on the bulk …
has been performed using direct numerical simulation. Mach numbers, based on the bulk …
Direct numerical simulation of impinging shock wave/turbulent boundary layer interaction at M= 2.25
S Pirozzoli, F Grasso - Physics of fluids, 2006 - pubs.aip.org
The interaction of a spatially developing adiabatic boundary layer flow at M∞= 2.25 and Re
θ= 3725 with an impinging oblique shock wave (β= 33.2) is analyzed by means of direct …
θ= 3725 with an impinging oblique shock wave (β= 33.2) is analyzed by means of direct …
[图书][B] Compressibility, turbulence and high speed flow
TB Gatski, JP Bonnet - 2013 - books.google.com
Compressibility, Turbulence and High Speed Flow introduces the reader to the field of
compressible turbulence and compressible turbulent flows across a broad speed range …
compressible turbulence and compressible turbulent flows across a broad speed range …
Advances in CFD prediction of shock wave turbulent boundary layer interactions
D Knight, H Yan, AG Panaras, A Zheltovodov - Progress in Aerospace …, 2003 - Elsevier
The paper presents a summary of recent computational fluid dynamics (CFD) simulations of
shock wave turbulent boundary layer interactions. This survey was prepared as part of the …
shock wave turbulent boundary layer interactions. This survey was prepared as part of the …
Direct simulation of the turbulent boundary layer along a compression ramp at M= 3 and Reθ= 1685
NA Adams - Journal of Fluid Mechanics, 2000 - cambridge.org
The turbulent boundary layer along a compression ramp with a deflection angle of 18° at a
free-stream Mach number of M= 3 and a Reynolds number of Reθ= 1685 with respect to free …
free-stream Mach number of M= 3 and a Reynolds number of Reθ= 1685 with respect to free …
Large-eddy simulation of shock-wave/turbulent-boundary-layer interaction
MS Loginov, NA Adams… - Journal of Fluid …, 2006 - cambridge.org
Well-resolved large-eddy simulations (LES) are performed in order to investigate flow
phenomena and turbulence structure of the boundary layer along a supersonic compression …
phenomena and turbulence structure of the boundary layer along a supersonic compression …
The approximate deconvolution model for large-eddy simulations of compressible flows and its application to shock-turbulent-boundary-layer interaction
A formulation of the approximate deconvolution model (ADM) for the large-eddy simulation
(LES) of compressible flows in complex geometries is detailed. The model is applied to …
(LES) of compressible flows in complex geometries is detailed. The model is applied to …