Numerical methods for high-speed flows

S Pirozzoli - Annual review of fluid mechanics, 2011 - annualreviews.org
We review numerical methods for direct numerical simulation (DNS) and large-eddy
simulation (LES) of turbulent compressible flow in the presence of shock waves. Ideal …

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 …

[图书][B] Large eddy simulation for compressible flows

E Garnier, N Adams, P Sagaut - 2009 - books.google.com
Page 1 E. Garnier N. Adams P. Sagaut SCIENTIFIC COMPUTATION Large Eddy Simulation
for Compressible Flows Springer Page 2 Large Eddy Simulation for Compressible Flows Page …

[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 …

Large-eddy simulation of low-frequency unsteadiness in a turbulent shock-induced separation bubble

E Touber, ND Sandham - Theoretical and computational fluid dynamics, 2009 - Springer
The need for better understanding of the low-frequency unsteadiness observed in shock
wave/turbulent boundary layer interactions has been driving research in this area for several …

A simple model for low-frequency unsteadiness in shock-induced separation

S Piponniau, JP Dussauge, JF Debieve… - Journal of Fluid …, 2009 - cambridge.org
A model to explain the low-frequency unsteadiness found in shock-induced separation is
proposed for cases in which the flow is reattaching downstream. It is based on the properties …

Space and time organization in a shock-induced separated boundary layer

P Dupont, C Haddad, JF Debieve - Journal of fluid Mechanics, 2006 - cambridge.org
The interaction of an oblique shock wave impinging on a turbulent boundary layer at Mach
number 2.3 is experimentally investigated for a wide range of shock intensities …

Unsteadiness in shock wave boundary layer interactions with separation

JP Dussauge, P Dupont, JF Debiève - Aerospace science and Technology, 2006 - Elsevier
Shock/turbulent boundary-layer interactions produce generally unsteadiness of the shock
system. This phenomenon is reviewed and analyzed, by evaluating the results of various …

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 …

High-order accurate, low numerical diffusion methods for aerodynamics

JA Ekaterinaris - Progress in Aerospace Sciences, 2005 - Elsevier
In recent years numerical methods have been widely used to effectively resolve complex
flow features of aerodynamics flows with meshes that are reasonable for today's computers …