Helicopter rotor model icing wind tunnel test method
A technology for helicopter rotor and wind tunnel testing, which is applied in the field of wind tunnel testing and can solve the problems that the experimental research has not been carried out effectively.
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[0034] Example
[0035] A wind tunnel test method for helicopter rotor model icing, such as figure 1 with figure 2 As shown, including the following steps:
[0036] Step 1. Each system of the rotor model test bench is debugged before the test. After each system works normally, go to step 2;
[0037] Step 2. When the rotor shaft inclination angle is zero, collect the zero reading as the initial reading. If the initial reading is correct, go to step 3;
[0038] Step 3. Start the safe operation of the rotor, then turn on the wind tunnel cooling system, and drive in the wind tunnel to cool down by adjusting the wind speed. During the cooling process, the rotor is operated in real time to keep the rotor lift, pitch and roll moments within a safe range. , After the wind tunnel ambient temperature drops to the test value and stabilizes, go to step 4;
[0039] Step 4: The rotor speed is increased to the test speed, and then the wind speed is adjusted to the test wind speed. During the wind ...
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