2019
DOI: 10.1109/access.2019.2949062
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Blended Wing Body Thrust Reverser Cascade Feasibility Evaluation Through CFD

Abstract: Airplane thrust reverser could significantly reduce the landing distance of a conventional civil turbofan. Control of the thrust reverser can be performed by a hydraulic and/or electric system. This study investigates whether this system can be used for blended wing body (BWB) civil airplanes as their engines are located over the wing body. Computational fluid dynamics (CFD) is used to analyze the feasibility of a thrust reverser cascade applied to BWB airplanes. This is selected because of its rapidity and lo… Show more

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Cited by 4 publications
(4 citation statements)
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“…We also performed a numerical analysis on the performance of the Bernoulli exhaust system for the 3D model of the disaster prevention comprehensive test site. As the first step in the numerical analysis process, we arranged a solid element for the 3D design [29]. After drawing the overall shape of the tunnel, we extracted the volume of the space where the flow occurred and designed the mesh [30].…”
Section: Computational Fluid Dynamics (Cfd) Numerical Analysis Methodsmentioning
confidence: 99%
“…We also performed a numerical analysis on the performance of the Bernoulli exhaust system for the 3D model of the disaster prevention comprehensive test site. As the first step in the numerical analysis process, we arranged a solid element for the 3D design [29]. After drawing the overall shape of the tunnel, we extracted the volume of the space where the flow occurred and designed the mesh [30].…”
Section: Computational Fluid Dynamics (Cfd) Numerical Analysis Methodsmentioning
confidence: 99%
“…The finite volume method was applied to solve the RANS equation, the second-order upwind Roe-FDS scheme was applied to discretize the inviscid spatial term, and the second-order central difference scheme was applied to discretize the viscid spatial term. The turbulence model used was the k-omega SST model (Menter, 1994) and the time-stepping method was the approximate factorization (AF) implicit time-marching method (Gang, Dong, Zhenli, & Zeyu, 2019). To accelerate convergence, the multi-grid method was applied.…”
Section: Methodsmentioning
confidence: 99%
“…The turbulence model used is k-omega SST model. The time-stepping method is an approximate factorization (AF) implicit time-marching method; the multigrid method is applied to accelerate the convergence process of calculation [25].…”
Section: The Aerodynamic Performance Of Swbmentioning
confidence: 99%