Results 371 to 380 of about 1,566,376 (417)
The Journal of the Royal Aeronautical Society, 1949 SummaryThe paper discusses the application of wind tunnels to aircraft design and consideration is given to the potentialities and limitations of types designed specifically for industrial use. Arguments affecting the choice of type, size and speed are stated and a detailed description is given of a particular tunnel which has very steady and even flow
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IEEE Computer Graphics and Applications, 1992
The design and implementation of a virtual environment linked to a graphics workstation for the visualization of complex fluid flows are described. The system user wears a stereo head-tracked display, which effectively displays 3-D information, and an instrumented glove to intuitively position flow-visualization tools.
Creon Levit, Stephen T. Bryson
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The design and implementation of a virtual environment linked to a graphics workstation for the visualization of complex fluid flows are described. The system user wears a stereo head-tracked display, which effectively displays 3-D information, and an instrumented glove to intuitively position flow-visualization tools.
Creon Levit, Stephen T. Bryson
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, 2017
Comprehensive wind tunnel experiments were carried out to study the interaction of a turbulent boundary layer with a wind turbine operating under different tip-speed ratios and yaw angles.
M. Bastankhah, F. Porté-Agel
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Comprehensive wind tunnel experiments were carried out to study the interaction of a turbulent boundary layer with a wind turbine operating under different tip-speed ratios and yaw angles.
M. Bastankhah, F. Porté-Agel
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The Wind at the End of the Tunnel
Environmental Science & Technology, 2000Although the world's growing appetite for wind energy is largely being fueled by European technology, a crucial wind tunnel test being conducted in the United States will benefit turbine developers everywhere.
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2020
Hypersonic wind tunnels are intended for studying the aerodynamics of hypersonic aircraft, space launchers, missiles, projectiles and the atmospheric re-entry of space vehicles.
Jean Délery +5 more
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Hypersonic wind tunnels are intended for studying the aerodynamics of hypersonic aircraft, space launchers, missiles, projectiles and the atmospheric re-entry of space vehicles.
Jean Délery +5 more
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Journal of the Soil Mechanics and Foundations Division, 1961
Modification of 19 ft pressure wind tunnel at Langley airfield so that it would operate under near vacuum conditions; necessary stiffening of steel tunnel shell doubled tunnel’s previous deadweight of 3000 tons; underpinning, needed by additional load, was provided by employing 2 types of piles with different stiffnesses and capacities.
J. S. O'Brien, J. F. McNulty
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Modification of 19 ft pressure wind tunnel at Langley airfield so that it would operate under near vacuum conditions; necessary stiffening of steel tunnel shell doubled tunnel’s previous deadweight of 3000 tons; underpinning, needed by additional load, was provided by employing 2 types of piles with different stiffnesses and capacities.
J. S. O'Brien, J. F. McNulty
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Sustainable Cities and Society, 2016
Abstract A novel wind tunnel with conical and elevation structure is proposed and demonstrated for power generation. A sucking fan is placed at the wind tunnel front end to simulate wind in the atmosphere and a wind turbine is placed at the backend of the wind tunnel to generate electricity.
Ahmad Atieh +2 more
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Abstract A novel wind tunnel with conical and elevation structure is proposed and demonstrated for power generation. A sucking fan is placed at the wind tunnel front end to simulate wind in the atmosphere and a wind turbine is placed at the backend of the wind tunnel to generate electricity.
Ahmad Atieh +2 more
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Slat Noise: Aeroacoustic Beamforming in Closed-Section Wind Tunnel with Numerical Comparison
, 2016Experiments in closed-section wind tunnels are more suitable for comparisons with numerical results than corresponding experiments in open-section tunnels because well-defined boundary conditions far from the model can be established for the numerics ...
C. Pagani, D. S. Souza, M. Medeiros
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2020
Built by Gustave Eiffel, and still in use, the low speed wind tunnel at the Scientific and Technical Centre for Building (CSTB) located in Auteuil was inaugurated on 19 March 1912 (see Fig. 2.1).
Patrick Gilliéron +5 more
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Built by Gustave Eiffel, and still in use, the low speed wind tunnel at the Scientific and Technical Centre for Building (CSTB) located in Auteuil was inaugurated on 19 March 1912 (see Fig. 2.1).
Patrick Gilliéron +5 more
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Progress in Aerospace Sciences, 1992
Abstract Until recently engineers have been unable to reach full scale Reynolds number in most wind tunnel tests. The cryogenic wind tunnel has been introduced to provide the aerospace community with the means to test models at near-full-scale Reynolds numbers, satisfying a particular need at transonic speeds.
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Abstract Until recently engineers have been unable to reach full scale Reynolds number in most wind tunnel tests. The cryogenic wind tunnel has been introduced to provide the aerospace community with the means to test models at near-full-scale Reynolds numbers, satisfying a particular need at transonic speeds.
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