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https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19730010542.pdf
WIND TUNNEL INTERFERENCE FACTORS FOR HIGH-LIFT WINGS IN CLOSED WIND TUNNELS Robert Glenn Joppa SUMMARY A problem associated with the wind tunnel testing of very slow flying aircraft is the correction of observed pitching moments to free air conditions. The most significant effects of such corrections are to be found at moderate downwash an-
https://repository.up.ac.za/bitstream/handle/2263/43061/Chen_Support_2014.pdf;sequence=1
The support system and support interference becomes one of the main investigation areas of experiment aerodynamics. Researchers have began their study on the support system and support interference after the first wind tunnel was built. In China, most of this works focused on the support system used for the aircraft featuring low aspect ration ...
http://www.icas.org/ICAS_ARCHIVE/ICAS2010/PAPERS/053.PDF
support. Comparison against experimental measurements thanks to dummy sting tests is provided for validation purpose. 1 Introduction During wind tunnel tests the aircraft model is maintained in the test section thanks to a support system. This support is shaped to …
https://www.researchgate.net/publication/303902425_Wind_Tunnel_Support_System_Influence_on_NASA_Common_Research_Model_at_Low_Speed_Conditions
The wind tunnel support system’s size is determined by the fact that substantial structures are needed in order to precisely orient the model under the influence of possibly significant ...
https://www.nasa.gov/centers/langley/news/factsheets/windtunnels.html
FS-2001-04-64-LaRC: Wind Tunnels at NASA Langley Research Center. The first major U.S. Government wind tunnel became operational in 1921 and was located at the Langley Memorial Aeronautical Laboratory of the National Advisory Committee for Aeronautics (NACA), which became NASA Langley Research Center in 1958. This wind tunnel was crude when compared to the tunnels …
https://www.nasa.gov/sites/default/files/643640main_SafetyManual.pdf
Jan 26, 2006 · Wind Tunnel Operations Division and Support Contractor Safety Manual A027-9991-XS1 Revision 7 January 26, 2006 This is a controlled document. Printed copies are for reference only.
http://www.aerofms.com/model_position
The Crescent Sting Support is designed to support the model weight and the aerodynamic loads generated by models with the least possible flow interference. The system is provided as a unit, allowing easy removal to accommodate other support systems in the test section or for maintenance.
https://en.wikipedia.org/wiki/Wind_tunnel
Wind tunnel modeling is accepted as a method for aiding in Green building design. For instance, the use of boundary layer wind tunnel modeling can be used as a credit for Leadership in Energy and Environmental Design (LEED) certification through the U.S. Green Building Council.
https://www.downloadcloud.com/wind-tunnel-simulator.html
The way that air flows around objects like cars, buildings, and certain products will have an impact on the outcome performance of the object. Hence designers will have to visualize this flow when designing. It can be done with the help of wind tunnel simulator online or wind tunnel simulator download. These aerodynamics simulation software will help in visualizing the flow and are easy to use.
https://www.researchgate.net/publication/230271809_Fundamentals_of_Wind-Tunnel_Design
Wind tunnels offer an effective tool to rapidly obtain data associated with flow over scaled or full-scale models. Given their ubiquitous nature and utility, a wind-tunnel design project is a ...
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