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Rocket "Angara" model tests in wind tunnel* T-117


Short-haul aircraft MC-21 model tests in wind tunnel T-102.


Orbiter "Express MD-1" tests in the acoustic reverberant chamber RK-1500.


Aircraft Yak-130 model nose-spin tests in the vertical wind tunnel T-105.


Short-haul aircraft MC-21 half-model tests on aeroelasticity in wind tunnel T-103.


Cathedral mosque model tests in wind tunnel T 1-2.
The Mosque was built in Moscow on the avenue Prospect Mira.


Planning parachute tests in wind tunnel T-101.


Counter-rotating turbine "screw" aircraft engine tests in wind tunnel T-104 on the DREAM project.


Section of bridge through Bosporus east on the island Russky model tests in wind tunnel T-103.


Short-haul aircraft MC-21 model icing tests in wind tunnel T-106.


Short-haul aircraft MC-21 tests in wind tunnel T-128.


Moscow City building "Federation" model tests in wind tunnel T 1-2.


Aircraft SSJ-100 model tests in wind tunnel T-104.


Aircraft SSJ-100 model buffet tests in wind tunnel T-103.


Live aircraft SSJ-100 in the static test hall.


Aircraft TU-334 in the static test hall.


An-225 Mria and space shuttle group model in the wind tunnel.


Short-haul aircraft model in wind tunnel T-106.


Helicopter model flow tests in the hydrodynamic tunnel.


Amphibious aircraft A-40 model tests in the towing basin at TSAGI.


Amphibious aircraft A-40 model tow [draft] tests in the towing basin at TSAGI


NASP "Buran" model at hyper-acoustic speed testing in wind tunnel T-117


Aerodynamic flutter tests in the wind tunnel


Aircraft MIG-29 in the subsonic wind tunnel T-101


Static tests hall


Aircraft aerodynamic research in the vertical wind tunnel T-105


Aircraft IL-114 model in the subsonic wind tunnel T-101


Pilot-training six-axis simulator complex


Supersonic wind tunnel T-128

A wind tunnel is a research tool used in aerodynamic research. It is used to study the effects of air moving past solid objects.
Wind tunnels were first proposed as a means of studying vehicles (primarily airplanes) in free flight. The wind tunnel was envisioned as a means of reversing the usual paradigm: instead of the air being still and the aircraft moving through it at speed, the same effect would be obtained if the aircraft stood still and the air moved past it at speed. In that way a stationary observer could study the aircraft in action, and could measure the aerodynamic forces being imposed on the aircraft.

Later, wind tunnel study came into its own: the effects of wind on man-made structures or objects needed to be studied, for example, when buildings became tall enough to present large surfaces to the wind, and the resulting forces had to be resisted by the building's internal structure. Determining such forces was required before building codes could specify the required strength of such buildings.

Still later, wind-tunnel testing was applied to automobiles, not so much to determine aerodynamic forces per se but more to determine ways to reduce the power required to move the vehicle on the roadway at a given speed. In these studies, the interaction between the road and the vehicle plays a significant role, and this interaction must be taken into consideration when interpreting the test results. In an actual situation, the roadway is moving relative to the vehicle but the air is stationary relative to the roadway, but in the wind tunnel the air is moving relative to the roadway, while the roadway is stationary relative to the test vehicle. Some automotive-test wind tunnels have incorporated moving belts under the test vehicle in an effort to approximate the actual condition.


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© 2012 by TsAGI


© 2012 by TsAGI