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https://commonresearchmodel.larc.nasa.gov/files/2018/01/AIAA-2016-3655.pdf
(a) CAD (b) CFD Figure 2. Support system The wind tunnel model used in the ETW is a 2.7% scale model of the CRM with a wingspan of 1.586m. The model’s horizontal tailplane was set to the neutral position (0 ) and no nacelles were mounted on the wings.
https://apps.dtic.mil/dtic/tr/fulltext/u2/a210614.pdf
to evaluate the aerodynamic influence of each support type on the model. Each support system configuration was attached to the facility High-Angle Automated Sting (HAAS) support system in Tunnel 16T and the High Pitch Sting Support System in Tunnel 16S. A representation
https://wmich.edu/mechanical-aerospace/advanced-windtunnel
The AAL took over the Advanced Design Wind Tunnel (ADWT) from the former McDonnell Douglas Aircraft Company (now the Boeing Company at St. Louis) and had it installed at the current location since 1999. The ADWT provides the opportunity for fundamental aerodynamic studies and efficient ...
https://www1.grc.nasa.gov/historic-facilities/altitude-wind-tunnel/awt-support-buildings/
In 1945, a supersonic wind tunnel with an 8-foot-long, 4-inch-wide and 10-inch-high test section was built in a passageway in the basement of the Shop and Office Building. Like the Stack Tunnels, the Duct Lab took advantage of the AWT’s exhaust system to produce its …
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://www.onera.fr/en/windtunnel/model-support
Twin sting support. The desire to measure the component of total drag attributed to an aircraft's tail assembly, together with the continuing need for better model support corrections, has brought about the design and implementation of twin-sting support for the wind tunnel. This support system was first installed in the S2MA wind tunnel during ...
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