Searching for Wind Tunnel Model Support System information? Find all needed info by using official links provided below.
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://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://www.onera.fr/en/windtunnel/model-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 1993.
https://wmich.edu/mechanical-aerospace/advanced-windtunnel
Model Support and Traverse Systems. ... Traverse system of two degrees of freedom for probes; Figure 4. The Advanced Design Wind Tunnel Returning Section and Motor. Applications. The ADWT is used for measurements of forces and moments, pressure fields and flow fields on and about relatively small aerodynamic models.
https://trace.tennessee.edu/cgi/viewcontent.cgi?article=6645&context=utk_gradthes
generic model support system that closely represents a typical wind tunnel model support system (sting, balance, and a generic model), measure the vibration in the model support system, perform modal analysis, and compare the results with finite element modeling. Passive damping techniques were also explored experimentally.Author: Kristi D Holland
https://apps.dtic.mil/dtic/tr/fulltext/u2/a210614.pdf
A wind tunnel investigation was conducted using a fighter aircraft model with various sting and blade support system arrangements to evaluate the effects of the mode] support sys- tem on the total body and component longitudinal force and moment data.
https://www.calspan.com/services/force-measurement-systems/model-positioning-systems/
Model Positioning Systems. During most of our history, we were collocated with the San Diego Low Speed Wind Tunnel. That experience, along with providing test support in many facilities across the US, gave us invaluable experience in wind tunnel operations.
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