2006
DOI: 10.1016/j.jcp.2006.02.009
|View full text |Cite
|
Sign up to set email alerts
|

Predicting shock dynamics in the presence of uncertainties

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3

Citation Types

0
32
0

Year Published

2010
2010
2017
2017

Publication Types

Select...
5
5

Relationship

0
10

Authors

Journals

citations
Cited by 52 publications
(32 citation statements)
references
References 15 publications
0
32
0
Order By: Relevance
“…(1) with Monte Carlo simulations (MCS) [11,12] and stochastic finite elements [13][14][15][16][17][18]. For transient nonlinear systems such as (1) these direct approaches are computationally expensive, and often prohibitively so, especially when the parameter fields have small correlation lengths and high variances.…”
Section: Introductionmentioning
confidence: 99%
“…(1) with Monte Carlo simulations (MCS) [11,12] and stochastic finite elements [13][14][15][16][17][18]. For transient nonlinear systems such as (1) these direct approaches are computationally expensive, and often prohibitively so, especially when the parameter fields have small correlation lengths and high variances.…”
Section: Introductionmentioning
confidence: 99%
“…In this more general case, the solution of linear hyperbolic problems may have lower regularity than those of elliptic, parabolic and hyperbolic problems with constant random coefficients. There are also recent works on stochastic nonlinear conservation laws, see for instance [25,26,34,39,40].…”
Section: Introductionmentioning
confidence: 99%
“…For this problem, they have also derived a collocation technique that reduces the computational burden associated with high-order non-linearities. Some research work in the supersonic regime have also been performed by Lin et al [12] dealing with 2D Euler equations for a stochastic wedge flow (random inflow velocity and random oscillations of the wedge around its apex). Loeven et al [13] make use of a deterministic compressible RANS code which is coupled to a probabilistic collocation solver to propagate freestream aerodynamic (Mach number) uncertainty through a subsonic steady flow around a NACA0012 airfoil.…”
Section: Introductionmentioning
confidence: 99%