Brownout Simulations of Model-Rotors In Ground Effect

In this work computational fluid dynamics is used to validate experimental results for a two-bladed small rotor In Ground Effect conditions. The paper focuses on the evaluation and prediction of the rotor outwash generated in ground effect. Time-averaged outflow velocities are compared with experime...

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Main Authors: Rovere F., Barakos G.N., Steijl R.
Format: Article
Language:English
Published: EDP Sciences 2020-01-01
Series:MATEC Web of Conferences
Online Access:https://www.matec-conferences.org/articles/matecconf/pdf/2020/10/matecconf_icsc-isatech20_01006.pdf
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author Rovere F.
Barakos G.N.
Steijl R.
author_facet Rovere F.
Barakos G.N.
Steijl R.
author_sort Rovere F.
collection DOAJ
description In this work computational fluid dynamics is used to validate experimental results for a two-bladed small rotor In Ground Effect conditions. The paper focuses on the evaluation and prediction of the rotor outwash generated in ground effect. Time-averaged outflow velocities are compared with experimental results, and the simulated flow field is used for safety studies using the PAXman model and particle tracking methods. The aircraft weights have been studied, evaluating scaling factors to define how helicopter weight can affect the outflow forces and the particle paths. Results show how the wake generated by heavier helicopters can lead to stronger forces on ground personnel and push the particles farther away from the rotor.
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spelling doaj.art-b5d4963ba0cd4da08b45040320a308262022-12-21T22:37:55ZengEDP SciencesMATEC Web of Conferences2261-236X2020-01-013140100610.1051/matecconf/202031401006matecconf_icsc-isatech20_01006Brownout Simulations of Model-Rotors In Ground EffectRovere F.0Barakos G.N.1Steijl R.2CFD Laboratory School of Engineering, University of GlasgowCFD Laboratory School of Engineering, University of GlasgowCFD Laboratory School of Engineering, University of GlasgowIn this work computational fluid dynamics is used to validate experimental results for a two-bladed small rotor In Ground Effect conditions. The paper focuses on the evaluation and prediction of the rotor outwash generated in ground effect. Time-averaged outflow velocities are compared with experimental results, and the simulated flow field is used for safety studies using the PAXman model and particle tracking methods. The aircraft weights have been studied, evaluating scaling factors to define how helicopter weight can affect the outflow forces and the particle paths. Results show how the wake generated by heavier helicopters can lead to stronger forces on ground personnel and push the particles farther away from the rotor.https://www.matec-conferences.org/articles/matecconf/pdf/2020/10/matecconf_icsc-isatech20_01006.pdf
spellingShingle Rovere F.
Barakos G.N.
Steijl R.
Brownout Simulations of Model-Rotors In Ground Effect
MATEC Web of Conferences
title Brownout Simulations of Model-Rotors In Ground Effect
title_full Brownout Simulations of Model-Rotors In Ground Effect
title_fullStr Brownout Simulations of Model-Rotors In Ground Effect
title_full_unstemmed Brownout Simulations of Model-Rotors In Ground Effect
title_short Brownout Simulations of Model-Rotors In Ground Effect
title_sort brownout simulations of model rotors in ground effect
url https://www.matec-conferences.org/articles/matecconf/pdf/2020/10/matecconf_icsc-isatech20_01006.pdf
work_keys_str_mv AT roveref brownoutsimulationsofmodelrotorsingroundeffect
AT barakosgn brownoutsimulationsofmodelrotorsingroundeffect
AT steijlr brownoutsimulationsofmodelrotorsingroundeffect