Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1997-06-10
1999-02-23
Dombroske, George
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
73178R, G01M 900
Patent
active
058746714
ABSTRACT:
An instrumented device for the study of airflow over a structure (10), comprises a support (16) forming a thin plate (24) adapted to be applied and shaped to the contour of a predetermined region of the structure. Connection structure (22) cements a portion of an inner surface of the support to that predetermined region, leaving a space (36) of low height between an inner surface of the plate (24) of the support and that predetermined region. This height is substantially equal to the thickness of said cementing structure. Instrumentation (18) is connected to the support, a portion (28) of this instrumentation and wire connections (20) therefor being disposed in that space (36), whereby the device is adapted to form a skin on the structure.
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Aerospatiale - Societe Nationale Industrielle
Amrozowicz Paul D.
Dombroske George
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