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Analizy CFD rozkładu kropel rozprzestrzenianych za pomocą statku powietrznego
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Abstrakty
The article describes a computational study, using CFD models, of droplet spray dispersal in the wake of a ‘Turbo Kruk’ airplane up to 500 m downstream. The CFD Reynolds-averaged Navier-Stokes (RANS) models use a Lagrangian (droplet phase) and Eulerian (fluid phase) procedure to predict the droplet trajectories trough the turbulent aircraft wake. The methods described in the work have the potential to improve current models for aerial spraying and will help in the development of new spraying procedures. In this study, the CFD models are used to describe the phenomenon of sprays released from atomizers mounted on the plane. A parametric study of the aircraft model examines the effects of crosswind on the aircraft’s vortex structures and the resulting droplet trajectories. The study shows, that such influence is underestimated in the current models. A comparison of the present results to AGDISP predictions is provided.
W artykule opisano analizy numeryczne, wykorzystujące współczesne metody CFD, do badania przestrzennego rozkładu kropel cieczy, rozpylonych w polu prędkości samolotu ‘Turbo Kruk’ w odległości do 500 m za statkiem powietrznym. Wykorzystano równania RANS, celem rozwiązania zagadnienia Lagrangea trajektorii kropel (dyskretnych cząstek) w powietrzu (płyn), rozumianym jako sturbulizowany ślad aerodynamiczny samolotu. Wybrana i opisana metoda w pracy posiada ogromny potencjał, możliwy do wykorzystania w celu ulepszenia obecnych, obowiązujących modeli opryskiwania z samolotu i ustalenia lepszych procedur technologicznych. W pracy wykorzystano metody CFD do opisania i analizy zjawiska rozpylania kropel przez atomizery, zamocowane na płatowcu. Podjęto problem wpływu wiatru bocznego na struktury wirowe, generowane lecącym statkiem powietrznym, a przez to na trajektorie kropel i rozkład przestrzenny masy oprysku. Pokazano, że taki wpływ jest niedoszacowany według obecnych, standardowych modeli, przede wszystkim poprzez porównanie do wyników uzyskanych w oparciu o model AGDISP.
Czasopismo
Rocznik
Tom
Strony
66--92
Opis fizyczny
Bibliogr. 48 poz., rys., tab., wykr., wzory
Twórcy
autor
- Polish Air Force Academy, ul. Dywizjonu 303 35, 08-521 Dęblin, Poland
autor
- Centre of New Technologies, Institute of Aviation, al. Krakowska 110/114, 02-256 Warsaw, Poland
autor
- Design Analysis & Calculation Group, PZL „Warszawa–Okęcie” S. A. Airbus Defence & Space, al. Krakowska 110/114, 02-256 Warsaw, Poland
Bibliografia
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- [35] Seredyn, T.P., 2014, “Experimental Investigations of a Drifting Cloud of Droplets Dispersed from Aircraft”, Archive of Mechanical Engineering, No. 3, pp. 393-407.
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- [41] Teske, M. E., Thistle, H. W., Schou, W. C., Miller, P. C. H., Strager, J. M., Richardson, B., Butler, M. C., Barry, J. W., Twardus, D. B. and Thompson, D. G., 2011b, “A Review of Computer Models for Pesticide Deposition Prediction”, Trans. ASAE No. 54(3), pp. 789-801.
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Uwagi
PL
Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2018).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-cdb1ea29-fe33-4a49-95b8-e170945f8a14