The invention provides a rotor type aircraft water landing
model test method. Firstly, a test device is installed, and electrical
signal connection and test are completed. Then, a hydrodynamic high
speed test trailer moves in an
orbit and drives a model to move, when the speed of the model reaches the running speed required by the test and is stable,
data acquisition equipment is started, after the normal working of the
data acquisition equipment is determined, a model connection component is controlled to loosen the model, and the model freely separates and goes into water to slide. After the model goes into the water, the hydrodynamic high
speed test trailer brakes and slows down until parking. After the test process is ended, the effectiveness of collected
test data is analyzed, valid test parameters are recorded, and the valid test parameters comprises model weight, center of gravity,
forward speed and sinking speed at the instant of going into water, a
pitch angle, a roll angle and a
yaw angle in a model initial state, and a
pitch angle, a roll angle and a
yaw angle, overload of center of gravity,
cockpit overload,
bottom pressure of the model after the model goes into the water. According to the method, a reliable basis is provided for effectively evaluating the water
landing performance of a rotor type aircraft.