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NÁVRH A KONŠTRUKCIA MODELU DEMONŠTRAČNÉHO AERODYNAMICKÉHO TUNELA
(Žilinská univerzita v Žiline, 2020)
The paper is focused on the creation of a fully functional demonstrational model of a subsonic wind tunnel with integrated accessories, using low air velocities to perform test analyses. The analyses take place in the form ...
Study of reinforcement design h-profile of aircraft wing spar
(University of Zilina, 2020)
In today's world, with ever-increasing safety requirements, there is a growing demand to maintain or reduce production costs. In aviation, in addition to factors like weight and related variables such as resistance to ...
Experimental state of thrust testing of aircraft reciprocating internal combustion engine
(University of Zilina, 2020)
The project “Experimental State of Thrust Testing of Aircraft Reciprocating Internal Combustion Engine” is aimed at creating a complex measuring device in order to obtain selected characteristics and parameters of the ...
Design procedure and honeycomb screen implementation to the air transtport department’s subsonic wind tunnel
(University of Zilina, 2020)
Wind tunnels are the most widely used tools when comes to validation of Reynold number. Most of wind tunnels use various air straighteners or flow conditioners to achieve as most unified air flow as it’s possible. This ...