System and method for measuring deformation of an object in...

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

Reexamination Certificate

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Reexamination Certificate

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07997130

ABSTRACT:
A monitoring system for monitoring a test article includes a scanning system and a computer system. The test article may be positioned within a fluid tunnel. The scanning system may be configured to scan the test article and record positional data of at least one point on an article surface of the test article. The computer system is in communication with the scanning system for receiving the positional data and being operative to determine at least one of the following: a position of the test article, an attitude of the test article, and deformation of the article surface.

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patent: 5020364 (1991-06-01), Manitt et al.
patent: 5345818 (1994-09-01), Magill et al.
patent: 7254998 (2007-08-01), Rueger
Charles V. Spain, “Assessing Videogrammetry for Static Aeroelastic Testing of a Wind-Tunnel Model,” 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Palm Springs, California, Apr. 19-22, 2004.
Wim Ruyten, “Model Attitude Measurement with an Eight-Camera Pressure-Sensitive Paint System,” 38th Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan. 10 -13, 2000.

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