The invention provides a continuous
pressure measurement test
system for a model surface based on a scanning valve, comprising a main control
machine and a plurality of pressure scanning valves, and also comprising a
system processor, an
optical fiber interface unit, a scanning valve
digital interface unit, a scanning valve interface unit, and a plurality of pressure calibration units. The systemprocessor is electrically connected to the
optical fiber interface unit and the plurality of pressure calibration units respectively. The
optical fiber interface unit communicates with the scanning valve
digital interface unit by optical fibers. The scanning valve
digital interface unit is connected to a plurality of pressure scanning valves through the scanning valve interface unit. The continuous
pressure measurement test
system can realize continuous collection of the
pressure data in a model movement process, so that a series of
pressure data from a range of
machine angle changes can be obtained in just one experiment. Moreover, sufficient intensive aerodynamic characteristic data can be collected in the process of the constant change of the attitude angle of the model, which greatly improves the efficiency of the wind tunnel
pressure measurement test, provides more complete and rich aerodynamic data, improves the
test efficiency, and reduces the test cost.