Numerical modeling of RDE

• Autorzy: Folusiak Michal , Swiderski Karol , Wolanski Piotr

Identyfikatory

DOI

10.2478/tar-2020-0019

Warianty tytułu

PL

Modelowanie numeryczne silnika z wirującą detonacją

• Języki publikacji: EN

Abstrakty

EN

The idea of using the phenomenon of rotating detonation to propulsion has its roots in fifties of the last century in works of Adamson et al. and Nicholls et al. at the University of Michigan. The idea was recently reinvented and experimental research and numerical simulations on the Rotating Detonation Engine (RDE) are carried in numerous institutions worldwide, in Poland at Warsaw University of Technology (WUT) since 2004. Over the period 2010-2014 WUT and Institute of Aviation (IOA) jointly implemented the project under the Innovative Economy Operational Programme entitled ‘Turbine engine with detonation combustion chamber’. The goal of the project was to replace the combustion chamber of turboshaft engine GTD-350 with the annular detonation chamber. This paper is focused on investigation of the influence of a geometry and flow conditions on the structure and propagation stability of the rotating detonation wave. Presented results are in majority an outcome of the aforementioned programme, in particular authors’ works on the development of the in-house code REFLOPS USG and its application to simulation of the rotating detonation propagation in the RDE.

PL

Pomysł wykorzystania zjawiska wirującej detonacji do napędu był po raz pierwszy rozważany w latach pięćdziesiątych ubiegłego wieku przez zespoły badawcze Adamsona i Nichollsa na Uniwersytecie Michigan. Badania nad silnikiem z detonacyjną komorą spalania zostały wznowione po blisko 40 latach i dziś prace prowadzone są w wielu jednostkach naukowych na świecie, a w Polsce na Politechnice Warszawskiej od 2004 roku. W latach 2010-2014 Instytut Lotnictwa oraz Politechnika Warszawska wspólnie realizowały projekt w ramach Programu Operacyjnego Innowacyjna Gospodarka ‘Silnik Turbinowy z detonacyjną komorą spalania’. Projekt zakłada zastąpienie komory spalania turbowałowego silnika GTD-350 pierścieniową komorą detonacyjną. Artykuł skupia się na badaniach numerycznych wpływu geometrii oraz parametrów przepływu na strukturę i stabilność propagacji wirującej detonacji. Przedstawione wyniki są w większości wynikiem prac autorów nad rozwojem kodu REFLOPS USG w czasie trwania projektu i koncentruje się na rozwoju i implementacji wysokowydajnych metod symulacji silnika z detonacyjną komorą spalania oraz ich zastosowaniu w symulacjach numerycznych propagacji wirującej fali detonacyjnej w silniku RDE.

Słowa kluczowe

EN

RDE; CFD; modeling; detonation; numerical

PL

silnik RDE; CFD; wirująca detonacja; modelowanie numeryczne

• Wydawca: Wydawnictwa Naukowe Sieci Badawczej Łukasiewicz - Instytutu Lotnictwa
• Czasopismo: Transactions on Aerospace Research
• Rocznik: 2020
• Tom: Nr 4 (261)
• Strony: 13--47
• Opis fizyczny: Bibliogr. 41 poz., rys., tab., wykr., wzory

Twórcy

autor

Folusiak Michal

• Gexcon AS, Norway

autor

Swiderski Karol

• SST SwissSafeTech AG, Switzerland

autor

Wolanski Piotr

• Łukasiewicz Research Network – Institute of Aviation, Al. Krakowska 110/114, 02-256 Warsaw

Bibliografia

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Uwagi

1. The authors want to express their thanks and gratitude to Prof. Piotr Wolanski, for scientific and technical leadership throughout the project. True appreciation for our former colleagues involved in RDE works, namely Dr Arkadiusz Kobiera, Prof. Jan Kindracki, Dr Pawel Surmacz, Dr Grzegorz Rarata,, Dr Borys Lukasik, Dr Dominik Kublik, Kamil Sobczak and Dr Michal Kawalec

2.Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2021).