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Zbornik radova Koridor 10 - Kirilo Savić

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3rd International Scientific and Professional Conference<br />

CORRIDOR <strong>10</strong> - a sustainable way of integrations<br />

RESEARCH SOME AERODYNAMICS PHENOMENON OF HIGH-<br />

SPEED TRAINS IN LOW-SPEED WIND TUNNEL<br />

Mirjana Puharić, Ph.D, Institute <strong>Kirilo</strong> Savić, , Belgrade, Serbia<br />

Vojkan Lučanin, M.Sc., Faculty of mechanical engineering, Belgrade University, Serbia<br />

Suzana Linić, B.Sc, Institute GOŠA, Belgrade, Serbia<br />

Dušan Matić, B.Sc, Institute GOŠA, Belgrade, Serbia<br />

ABSTRACT<br />

This paper describes the use of low-speed aerodynamic tunnel testing of phenomena that occur<br />

during movement of trains.<br />

The first part of the study include experimental research of model trains, carried out in low speed wind<br />

tunnel. Model train, which was made in scale 1:20, was tested. The aerodynamic pressure on the train<br />

model, which is generated by the movement of the train, was measured. Velocity of the train has been<br />

180 km/h. Research contains measurement of the pressure distribution on the train model using holes<br />

for measuring pressure and pressure sensors. Pressure sensors are connected with multiplexer<br />

pressure type Scanivalve using plastic pneumatic tubes.<br />

The second part of this study includes numerical calculation using methods CFD - Computational Fluid<br />

Dynamics - Fluent. The numerical calculation is based on the finite volume technique. Fluent was<br />

used to predict the parameters of the flow field of high-speed train.<br />

The results of the experiment and pressures predicted by CFD for the same conditions were<br />

compared.<br />

Keywords: high-speed train, aerodynamic, wind tunnel, Fluent, pressure scanning system, differential<br />

pressure gauge, sensors for measuring pressure<br />

ISTRAŽIVANJE NEKIH AERODINAMIČKIH FENOMENA VOZOVA VELIKIH BRZINA U<br />

AERODINAMIČKOM TUNELU MALIH BRZINA<br />

U ovom radu opisana je primena aerodinamičkih tunela malih brzina u ispitivanjima fenomena koji se<br />

javljaju pri kretanju vozova.<br />

Prvi deo studije obuhvata eksperimentalna istraživanja modela voza, koja su izvršena u<br />

aerodinamičkom tunelu malih brzina. Ispitivan je model voza, izrađen u razmeri 1:20. Na modelu voza<br />

je meren aerodinamički pritisak nastao prolaskom voza. Brzina voza je 180 km/h. Istraživanja<br />

obuhvataju merenje raspodela pritisaka na modelu voza, pomoću rupica za merenje pritisaka i davača<br />

pritiska. Davači pritiska su pneumatskim cevčicama povezani sa multiplekserom pritisaka tipa<br />

Scanivalve.<br />

Drugi deo ovog ispitivanja obuhvata numerički proračun pomoću CFD metode, kompjuterska dinamika<br />

fluida – Fluent. Numerički proračun je zasnovan na tehnici konačnih zapremina. Fluent je korišćen za<br />

određivanje parametara strujnog polja kod voza velikih brzina.<br />

Rezultati eksperimenta su poređeni sa pritiscima dobijenim CFD metodom za iste uslove.<br />

Ključne reči: vozovi velikih brzina, aerodinamika, aerotunel, Fluent, sistem za merenje pritisaka,<br />

diferencijalni davač pritiska, senzori za merenje pritisaka<br />

Belgrade, 2012 220

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