发明名称 Crossflow vorticity sensor
摘要 A crossflow vorticity sensor is provided for the detection of crossflow vorticity characteristics. The crossflow vorticity sensor is comprised of crossflow sensors (10) which are non-invasively adhered to swept wing laminar surface (12) either singularly, in multi-element strips (11), in polar patterns (40), or orthogonal patterns (41). These crossflow sensors (10) are comprised of hot-film sensor elements (18) which operate as a constant temperature anemometer circuit to detect heat transfer rate changes. Accordingly, crossflow vorticity characteristics are determined via cross-correlation. In addition, the crossflow sensors (10) have a thickness which does not exceed a maximum value h in order to avoid contamination of downstream crossflow sensors (10).
申请公布号 US4727751(A) 申请公布日期 1988.03.01
申请号 US19870003676 申请日期 1987.01.15
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 HOLMES, BRUCE J.;CARRAWAY, DEBRA L.;HOLMES, HARLAN K.;MOORE, THOMAS C.
分类号 G01M9/06;G01P5/12;(IPC1-7):G01M9/00 主分类号 G01M9/06
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