14th WCCM-ECCOMAS Congress 2021
DOI: 10.23967/wccm-eccomas.2020.308
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Simulation of Helicopter Rotors On Unstructured Mixed Meshes Using Edge-Based Reconstruction Schemes

Abstract: The paper gives a detailed description of the developed numerical method for simulating the turbulent flow around a helicopter rotor and calculating its aerodynamic characteristics. The method is based on the original vertex-centered finite-volume EBR schemes. The features of these schemes are their higher accuracy that is achieved through the use of edge-based reconstruction of variables on extended quasi-one-dimensional stencils, and a moderate computational cost that allows for serial computations. When dea… Show more

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Cited by 2 publications
(3 citation statements)
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“…The aerodynamic characteristics of Caradonna-Tung rotor in hover simulated in the RFR were predicted in our previous work [13]. The results showed a good agreement with the experimental data for pressure coefficient distribution and the tip vortex trajectory.…”
Section: Aerodynamic Characteristics Of Isolated Rotorsupporting
confidence: 68%
See 1 more Smart Citation
“…The aerodynamic characteristics of Caradonna-Tung rotor in hover simulated in the RFR were predicted in our previous work [13]. The results showed a good agreement with the experimental data for pressure coefficient distribution and the tip vortex trajectory.…”
Section: Aerodynamic Characteristics Of Isolated Rotorsupporting
confidence: 68%
“…The hovering helicopter flight is modelled by the Caradonna-Tung rotor [10] and ROBIN fuselage [11,12], scaled to be compatible with the rotor radius. The choice of the helicopter model is motivated by the availability of detailed geometrical descriptions, experimental results, and prior experience simulating these separate cases [13].…”
Section: Introductionmentioning
confidence: 99%
“…In our simulations, meshes of up to 400 million nodes have been used so far. More information, including validation and comparison of RANS and DES results, can be found in [3,4]. Currently available supercomputer resources allow modeling only separate fragments of aircrafts.…”
Section: Applicationsmentioning
confidence: 99%