41st Aerospace Sciences Meeting and Exhibit 2003
DOI: 10.2514/6.2003-365
|View full text |Cite
|
Sign up to set email alerts
|

Near Field Trailing Edge Tone Noise Computation

Abstract: Blunt trailing edges in a flow often generate tone noise due to wall-jet shear layer and vortex shedding. In this paper, the spacetime conservation element and solution element (CE/SE) method is employed to numerically study the near-field noise of blunt trailing edges. Two typical cases, namely, flow past a circular cylinder (aeolian noise problem ) and flow past a flat plate of finite thickness are considered. The computed frequencies and the estimated sound pressure level (SPL) compare well with experimenta… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3

Citation Types

0
3
0

Year Published

2009
2009
2016
2016

Publication Types

Select...
5

Relationship

0
5

Authors

Journals

citations
Cited by 7 publications
(3 citation statements)
references
References 9 publications
0
3
0
Order By: Relevance
“…In recent years, another interesting ABC for finite volume (FV) schemes was discovered empirically, e.g., Leveque [6] and Loh et al [7][8][9][10]. When the flow conditions prescribed at the ghost cell centers (GCCs) do not match the flow within the domain, a matched layer similar to the one in the PML method is automatically captured at the boundary to do the matching, saving the work of creating a matched layer or matching the flow data.…”
Section: Introductionmentioning
confidence: 97%
“…In recent years, another interesting ABC for finite volume (FV) schemes was discovered empirically, e.g., Leveque [6] and Loh et al [7][8][9][10]. When the flow conditions prescribed at the ghost cell centers (GCCs) do not match the flow within the domain, a matched layer similar to the one in the PML method is automatically captured at the boundary to do the matching, saving the work of creating a matched layer or matching the flow data.…”
Section: Introductionmentioning
confidence: 97%
“…So far, the CE/ SE method has been mainly applied in numerical simulations of supersonic flows. Chang et al [15,[17][18][19][20][21][22][23][24][25][26] used this method for the aeroacoustic computations and studying the jet of nozzle; Guo et al [27] extended the CE/SE method to viscous flows; Yu et al [28][29][30][31] simulated chemical detonation waves by using the CE/SE method; and Zhang et al [32] derived the CE/SE scheme for MHD equations. However, the CE/SE method has not been employed to solve the complex elastic-plastic flows with solid features till now.…”
Section: Introductionmentioning
confidence: 99%
“…So far, the CE/SE method has been mainly applied in supersonic flow. Chang et al [24][25][26][27][28][29][30][31] adopted this method in aeroacoustic computation and the jet of nozzles; Guo et al [32] extended the CE/SE method to viscous flows; Yu and coworkers [33][34][35][36] simulated chemical detonation waves by the CE/SE method; and Zhang et al [37] derived the CE/SE scheme for MHD equations. Molls [1] employed the original CE/SE scheme to solve 1-D Saint-Venant equations, and the CE/SE scheme with a splitting technique, which cannot ensure the flux conservation, was utilized in 2-D shallow water equations.…”
Section: Introductionmentioning
confidence: 99%