2016
DOI: 10.2514/1.j054138
|View full text |Cite
|
Sign up to set email alerts
|

Validation of a High-Order Large-Eddy Simulation Solver Using a Vertical-Axis Wind Turbine

Abstract: A high-order implicit large-eddy simulation method in two dimensions and three dimensions is used to simulate the aerodynamics of a NACA0012 airfoil over large angles of attack at low chord Reynolds numbers (Re 5000-50;000). The two-dimensional code is found to have adequate agreement with lift and drag experimental data for prestall angles of attack, whereas the three-dimensional code is validated over all angles of attack. The three-dimensional method is able to accurately predict the magnitude and frequency… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1
1

Citation Types

0
8
0

Year Published

2016
2016
2023
2023

Publication Types

Select...
4
2
1

Relationship

2
5

Authors

Journals

citations
Cited by 11 publications
(8 citation statements)
references
References 40 publications
0
8
0
Order By: Relevance
“…where γ is the adiabatic gas constant. For the viscous problems, we introduce an isentropic assumption of the form p = Kρ γ , for a given constant K, as described in [17]. This additional simplification can be thought of as an artificial compressibility model for the incompressible flows simulated in Sections 5.2 and 5.3.…”
Section: Equations and Spatial Discretizationmentioning
confidence: 99%
See 1 more Smart Citation
“…where γ is the adiabatic gas constant. For the viscous problems, we introduce an isentropic assumption of the form p = Kρ γ , for a given constant K, as described in [17]. This additional simplification can be thought of as an artificial compressibility model for the incompressible flows simulated in Sections 5.2 and 5.3.…”
Section: Equations and Spatial Discretizationmentioning
confidence: 99%
“…Within each group, each process is then assigned to one stage of the IRK method. Thus, when assembling the block matrix of the form (17), the Jacobian matrices for all of the stages are computed in parallel. This does not require any communication between the groups.…”
Section: Stage-parallelism and Partitioned Ilumentioning
confidence: 99%
“…The determination of the actual α 0 used in the experiments is discussed in Ref. 12. We chose the static 'toe-out' angle of each of the airfoils α 0 to be 2 • , since it best matches the experimental data.…”
Section: Iib Model Turbinementioning
confidence: 99%
“…However, since the turbines rotate individually around their center axes, we cannot simply rotate the entire mesh like was done in the single turbine case in Ref. 12. Instead, we use the following moving-mesh strategy that incorporates rigid rotations that stretch the elements as well as techniques to change the element connectivities to prevent poor element qualities.…”
Section: Iiia Computational Domain and Moving Mesh Strategymentioning
confidence: 99%
“…Using eigenvalue analyses, it is possible to derive tight upper bounds on the condition number of (19) for all γ ∈ (0, ∞) when L is symmetric negative semi-definite (SNSD) or skew symmetric (SS) (see [4] for related derivations). These tight upper bounds achieve equality for all γ ∈ (0, ∞) as the spectrum of L becomes dense in [0, ∞) for SNSD L, and dense in (−i∞, i∞) for SS L. In each case, the tight upper bounds are minimized over all γ ∈ (0, ∞) when γ = γ * , for γ * given by (23), which is perhaps unsurprising given Corollary 1. At the minimum γ = γ * , the tight bound for the SNSD case is…”
mentioning
confidence: 91%