Method for establishing flight icing state space in flight icing simulator
A state space and simulator technology, applied in the field of flight simulators, which can solve problems that cannot cover flight, atmospheric conditions, and limited number of
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[0064] The principle of the method for establishing the flight icing state space in the flight icing simulator proposed by the present invention will be further described below with a specific embodiment. This implementation example is about the establishment of the state space for flight icing of two-dimensional NACA0012 wings in the flight icing simulator.
[0065] Known flight parameters:
[0066] Mach number M ∞ =0.35;
[0067] Reynolds number Re=4.8x10 6 ;
[0068] Known atmospheric parameters:
[0069] Liquid water content LWC=0.45(g / m 3 );
[0070] Average diameter MVD = 20 (μm);
[0071] The composition of the original sample space:
[0072] Under the above-mentioned flight conditions and atmospheric conditions, there are 8 atmospheric temperatures of 12, 15, 18, 20, 22, 25, and 28F. Calculated by computational fluid dynamics software, the icing state (position and shape) within 400 seconds uses a total of 1,420,000 spatial nodes, and a total of 1024 nodes on ...
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