8.6.- AERODYNAMICS

Aerodynamics is the part of fluid mechanics that studies the gases in motion and the forces or reactions to which the bodies that interact with those gases are subjected. Apart from the importance of aerodynamics in itself, the value of its contribution to aeronautics must be added. According to Mach number or the relative speed of a body in motion with respect to the air, the aerodynamics is divided into subsonic and supersonic according to whether that number is less than or greater than unity.

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In fluid mechanics, within the study of gases, air is normally used, being the main variables that are usually quantified the speed, pressure, drag force or lift force, etc. Wind tunnels are devices widely used in fluid mechanics tests to determine wind action on different types of bodies. The model to be studied remains at rest, while the flow is set in motion. The main parts of an aerodynamic tunnel are: the fan, the diffuser, the chamber, a contraction section and a test section.

Every time we move or throw an object, a number of physical principles that we do not normally notice act. Knowing the principles of aerodynamics is useful for a long list of activities, from the takeoff and piloting of a plane, to driving a vehicle or throwing a ball.

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AERODYNAMICS EQUIPMENT

1.- PHYSICS 2.- ELECTRONICS 3.- COMMUNICATIONS 4.- ELECTRICITY 5.- ENERGY 6.- MECHATRONICS & AUTOMATION 7.- MECHANICS 8.- FLUID MECHANICS 9.- THERMODYNAMICS & THERMOTECHNICS 10.- PROCESS CONTROL 11.- CHEMICAL ENGINEERING 12.- FOOD & WATER TECHNOLOGIES 13.- ENVIRONMENT 14.- BIOMEDICAL ENGINEERING LABORATORY ACCESSORIES CUSTOMIZED PILOT PLANTS
8.1.- FLUID MECHANICS MODULAR LABORATORY 8.2.- MEASUREMENT 8.3.- HYDROSTATICS 8.4.- FLOW VISUALIZATION 8.5.- HYDRAULIC CHANNELS 8.6.- AERODYNAMICS 8.7.- FLUID MACHINES 8.8.- FLUID PIPING SYSTEM 8.9.- INSTALLATIONS AND MAINTENANCE
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COMPUTER CONTROLLED SUPERSONIC WIND TUNNEL - TAS25/100C
  • TAS25/100C
Available
8.6.- AERODYNAMICS

TAS25/100C

Computer Controlled Supersonic Wind Tunnel

The Computer Controlled Supersonic Wind Tunnel, "TAS25/100C", is an open wind tunnel for the study of the aerodynamic properties of different drag bodies subject to subsonic and supersonic flows. Air flows through a vacuum pump or blower...
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COMPUTER CONTROLLED SUPERSONIC WIND TUNNEL (THREE BLOWERS) - TAS25/100C-3B
  • TAS25/100C-3B
Available
8.6.- AERODYNAMICS

TAS25/100C-3B

Computer Controlled Supersonic Wind Tunnel (Three Blowers)

The Computer Controlled Supersonic Wind Tunnel (Three Blowers), "TAS25/100C-3B", is an open wind tunnel for the study of theaerodynamic properties of different drag bodies subject to subsonic and supersonic flows.Airflows through three vacuum...
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COMPUTER CONTROLLED AERODYNAMIC TUNNEL, 50 X 250 MM - TA50/250C
  • TA50/250C
Available
8.6.- AERODYNAMICS

TA50/250C

Computer Controlled Aerodynamic Tunnel, 50X250 mm

The Computer Controlled Aerodynamic Tunnel, 50 x 250 mm, "TA50/250C", is a wind tunnel designed to study subsonic aerodynamics in a tunnel in open circuit and with incompressible subsonic flow. Air is drawn by a variable speed fan, computer...
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AERODYNAMIC TUNNEL, 50X250 MM - TA50/250
  • TA50/250
Available
8.6.- AERODYNAMICS

TA50/250

Aerodynamic Tunnel, 50X250 mm

The Aerodynamic Tunnel, 50 x 250 mm, "TA50/250", is a wind tunnel designed to study subsonic aerodynamics in a tunnel in open circuit and with incompressible subsonic flow. Air is drawn by a variable speed fan located at the discharge end of the...
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COMPUTER CONTROLLED AERODYNAMIC TUNNEL, 300 X 300 MM - TA300/300C
  • TA300/300C
Available
8.6.- AERODYNAMICS

TA300/300C

Computer Controlled Aerodynamic Tunnel, 300X300 mm

The Computer Controlled Aerodynamic Tunnel, 300 x 300 mm, "TA300/300C", is a wind tunnel designed to study subsonic aerodynamics in a tunnel in open circuit and with incompressible subsonic flow. Air is drawn by a variable speed fan, computer...
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AERODYNAMIC TUNNEL, 300 X 300 MM - TA300/300
  • TA300/300
Available
8.6.- AERODYNAMICS

TA300/300

Aerodynamic Tunnel, 300X300 mm

The Aerodynamic Tunnel, 300 x 300 mm, "TA300/300", is a wind tunnel designed to study subsonic aerodynamics in a tunnel in open circuit and with incompressible subsonic flow. Air is drawn by a variable speed fan located at the discharge end of the...
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COMPUTER CONTROLLED AERODYNAMIC TUNNEL, 610 X 915 MM - TA610/915C
  • TA610/915C
Available
8.6.- AERODYNAMICS

TA610/915C

Computer Controlled Aerodynamic Tunnel, 610X915 mm

Aerodynamics is the part of fluid mechanics that studies the motion of gases and the forces or reactions to which the bodies they interact with are subjected. Aerodynamics is not only important by itself but also as a complement to aeronautics....
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COMPUTER CONTROLLED AERODYNAMIC TUNNEL, 1000 X 1000 MM - TA1000/1000C
  • TA1000/1000C
Available
8.6.- AERODYNAMICS

TA1000/1000C

Computer Controlled Aerodynamic Tunnel, 1000X1000 mm

Aerodynamics is the part of fluid mechanics that studies the motion of gases and the forces or reactions to which the bodies they interact with are subjected. Aerodynamics is not only important by itself but also as a complement to aeronautics....
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COMPUTER CONTROLLED AERODYNAMIC TUNNEL, 1200X1200 MM - TA1200/1200C
  • TA1200/1200C
Available
8.6.- AERODYNAMICS

TA1200/1200C

Computer Controlled Aerodynamic Tunnel, 1200X1200 mm

Aerodynamics is the part of fluid mechanics that studies the motion of gases and the forces or reactions to which the bodies they interact with are subjected. Aerodynamics is not only important by itself but also as a complement to aeronautics....
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COMPUTER CONTROLLED CLOSED AERODYNAMIC TUNNEL, 2000X2000 MM - TACL2000/2000C
  • TACL2000/2000C
Available
8.6.- AERODYNAMICS

TACL2000/2000C

Computer Controlled Closed Aerodynamic Tunnel, 2000X2000 mm

Aerodynamics is the part of fluid mechanics that studies the motion of gases and the forces or reactions to which the bodies they interact with are subjected. Aerodynamics is not only important by itself but also as a complement to aeronautics....
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AERODYNAMIC TUNNEL FOR FLOW VISUALIZATION - TAVF180/100
  • TAVF180/100
Available
8.4.- FLOW VISUALIZATION

TAVF180/100

Aerodynamic Tunnel for Flow Visualization

The Flow Visualization Aerodynamic Tunnel, "TAVF180/100", designed by EDIBON, consists of a vertical conduction in which an upward flow of air and smoke is induced, which passes through different models allowing to study the behavior of the flow...
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AERODYNAMIC TUNNEL FLIGHT DEMONSTRATION UNIT - TADV225/450
  • TADV225/450
Available
8.6.- AERODYNAMICS

TADV225/450

Aerodynamic Tunnel Flight Demonstration Unit

The Aerodynamic Tunnel for Flight Demonstration, "TADV225/450", designed by EDIBON, consists of an open wind tunnel in whose working section the model of an aircraft with fixed wings is located. The aircraft is piloted by the user using controls...
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AERODYNAMIC TESTING BENCH - ATBB
  • ATBB
Available
8.6.- AERODYNAMICS

ATBB

Aerodynamic Testing Bench

The Aerodynamic Testing Bench, "ATBB", designed by EDIBON , has two main components: a radial fan with speed control and a working section where the different accessories for the tests are fixed.The radial blower impels the air through an air...
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