Method and device for improving accuracy of wind tunnel...

Measuring and testing – Wind tunnel: aerodynamic wing and propeller study

Reexamination Certificate

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Reexamination Certificate

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11316151

ABSTRACT:
A method for improving the precision of wind tunnel measurements provides a correction to reduce the influence of a suspension device. A model, such as an aircraft model, is held by the suspension device in a wind tunnel and has multiple suspension wires. By attaching one or more sleeves to each suspension wire, a plurality of measurements with identical model configuration are capable of providing data for extrapolating corrected measurement values for a plurality of aerodynamic characteristic variables measurable in a wind tunnel. Examples of sleeves include a slit along the sleeve length and an inner diameter of the sleeves selected such that the sleeve is capable of being pressed onto and removed from a suspension wire or a sleeve of lesser outer diameter.

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patent: 2768526 (1956-10-01), Trimble, Jr. et al.
patent: 3276251 (1966-10-01), Reed, III
patent: 4116056 (1978-09-01), Bulychev et al.
patent: 4920791 (1990-05-01), Griffin
patent: 5345818 (1994-09-01), Magill et al.
patent: 3-237335 (1991-10-01), None
patent: 7-301578 (1995-11-01), None
patent: 2002-323403 (2002-11-01), None

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