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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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