发明名称 Flow measurement device utilizing force transducers
摘要 A missile-shaped body is calibrated to determine characteristic influence coefficients. Thereafter, the body is positioned in a flow field where normal forces and pitch moments are measured. Due to the fact that influence coefficients are predetermined as a result of calibration, the force and moment measurements are used to solve equations for flow field angularity.
申请公布号 US4735085(A) 申请公布日期 1988.04.05
申请号 US19860898682 申请日期 1986.08.21
申请人 GRUMMAN AEROSPACE CORPORATION 发明人 MEYER, RUDOLPH C.
分类号 G01P13/02;(IPC1-7):G01C21/00;G01M9/00 主分类号 G01P13/02
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