Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1988-06-16
1989-09-05
Woodiel, Donald O.
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
G01M 900
Patent
active
048627399
ABSTRACT:
A wind tunnel model support mechanism has a double gimbal arrangement coupled to the tunnel's solid string, allowing the model freedom to move in all three major axes; pitch, roll and yaw with limited movement in horizontal and vertical displacement. Such a support enables evaluation of flutter characteristics not possible during conventional fixed sting operations.
REFERENCES:
patent: 2782636 (1957-02-01), Peucker
patent: 2864568 (1958-12-01), Ikard et al.
patent: 2955462 (1960-10-01), Holderer
Rockwell International Corporation
Silberberg Charles T.
Weston Harold C.
Woodiel Donald O.
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