Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1977-04-04
1978-08-22
Ruehl, Charles A.
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
73133R, G01M 900, G01L 516
Patent
active
041079868
ABSTRACT:
A five-component strain gauge balance for measuring the forces and moments exerted on a reflection plane model aircraft in a subsonic continuous-duty or blow down wind tunnel. The balance beams are arranged in a diamond pattern so that the rolling moment reactions are concentrated in the side beams making the axial force, normal force and yawing moment felt by the forward and aft beams more accurately measurable. The entire balance is machined from a single piece of material, ensuring maximum repeatability of measurements. This design also simplifies fabrication and provides better access for gauging.
REFERENCES:
patent: 2582814 (1952-01-01), Beman et al.
patent: 3618376 (1971-11-01), Shull et al.
Jason Walter J.
Kohlmann Henry G.
McDonnell Douglas Corporation
Royer Donald L.
Ruehl Charles A.
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