Aiming at the actuality that complexity of testing data and unable to carry out actual flight test during the aircraft wind tunnel tests

especially the thin-airfoil model has some characteristics

such as thin of itself

dense of surface test points and more test parameters which make test more difficult.Sensors’ structure and function and the theory of intelligent sensor system are studied by combining with much practical engineering practice.A new type of sensor array are designed

fabricated and calibrated.It is applied in actual aircraft’s aerodynamic parameters test system.