Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1999-06-18
2000-05-09
Raevis, Robert
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
G01L 516
Patent
active
060587695
ABSTRACT:
An assembly for positioning a measurement probe proximate a test body disposed for a fluid tunnel test includes a frame having a forward frame portion for attachment to a fluid flow tunnel fluid outlet, an aft frame portion aligned with the forward frame portion, and axial support members interconnecting the forward and aft frame portions. The assembly further includes a probe mount portion having a base slidably mounted on one or more of the axial support members, a probe supporting strut mounted on the base, and a probe mounted in the strut and movable in directions radially of the frame, and a probe moving member for moving the probe radially inwardly and outwardly of the frame portions.
REFERENCES:
patent: 4188822 (1980-02-01), Schoenherr et al.
patent: 5056361 (1991-10-01), Roberts
Kelly et al., "The General Motors Engineering Staff Aerodynamics Laborato-A Full-Scale Automotive Wind Tunnel"; SAE 820371; Feb. 22-26, 1982; SAE of Warrendale, PA; pp. 1-18.
Corriveau Pierre J.
Dooley Richard E.
Polhemus, Jr. Stanley J.
Wilkinson William S.
Kasischke James M.
Lall Prithvi C.
McGowan Michael J.
Raevis Robert
The United States of America as represented by the Secretary of
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