Method of forming micro-sensor thin-film anemometer
摘要
A device for measuring turbulence in high-speed flows is provided which includes a micro-sensor thin-film probe. The probe is formed from a single crystal of aluminum oxide having a 14 DEG half-wedge shaped portion. The tip of the half-wedge is rounded and has a thin-film sensor attached along the stagnation line. The bottom surface of the half-wedge is tilted upward to relieve shock induced disturbances created by the curved tip of the half-wedge. The sensor is applied using a microphotolithography technique.
申请公布号
US6018861(A)
申请公布日期
2000.02.01
申请号
US19960698559
申请日期
1996.08.15
申请人
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE UNITED STATES NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
发明人
SHEPLAK, MARK;MCGINLEY, CATHERINE B.;SPINA, ERIC F.;STEPHENS, RALPH M.;HOPSON, JR., PURNELL;CRUZ, VINCENT B.