2015
DOI: 10.2514/1.c033164
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Detached-Eddy Simulation of a Wide-Body Commercial Aircraft in High-Lift Configuration

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Cited by 16 publications
(9 citation statements)
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“…What is more, Waldmann et al [16], Lutz et al [17], and Zimmermann et al [18] numerically investigated the influence of unsteady wake on the tail of NASA CRM wing-body-tail configuration under poststall condition by the DDES method based on a TAU solver. Escobar et al [19] made use of the DES97 method in ANSYS Fluent to make a detailed analysis of the flow around the DLR-F11 high-lift configuration.…”
Section: Introductionmentioning
confidence: 99%
“…What is more, Waldmann et al [16], Lutz et al [17], and Zimmermann et al [18] numerically investigated the influence of unsteady wake on the tail of NASA CRM wing-body-tail configuration under poststall condition by the DDES method based on a TAU solver. Escobar et al [19] made use of the DES97 method in ANSYS Fluent to make a detailed analysis of the flow around the DLR-F11 high-lift configuration.…”
Section: Introductionmentioning
confidence: 99%
“…The numerical experiments are conducted using the solver ANSYS Fluent, which is commonly and successfully employed for building virtual wind tunnels in the industrial aerodynamics research, e.g. [ 11 14 ]. The present results are validated by comparison with reference experimental data that are provided by the industrial researchers.…”
Section: Introductionmentioning
confidence: 99%
“…The detailed air flow field is simulated by employing a fully three-dimensional CFD method, while following the Reynolds-averaged Navier-Stokes (RANS) approach. The numerical simulations are conducted using the solver ANSYS Fluent, which is commonly and successfully employed for building virtual wind tunnels in industrial aerodynamics research [ 5 8 ]. Indeed, this approach is followed in similar works investigating the aerodynamics of innovative regional aircraft models [ 9 , 10 ].…”
Section: Introductionmentioning
confidence: 99%