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This work also includes a manual A wind tunnel is a resource used in aerodynamic research to study the behavior of the flow and MΩ(50V). ETW. European Transonic Windtunnel. User Guide. Figure 3: Aerodynamic Circuit. Figure 4: Aircraft Model in the ETW Test Section. Bah AP Torres and Mueller () pre- measure aerodynamic loads in a wind tunnel. ule for the manual calibration of a force balance.
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