Zbornik radova Koridor 10 - Kirilo SaviÄ
Zbornik radova Koridor 10 - Kirilo SaviÄ
Zbornik radova Koridor 10 - Kirilo SaviÄ
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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