Method of obtaining wing installing angle of triphibian hovership
A technology of installation angle and acquisition method, applied in computer-aided design, special data processing applications, instruments, etc., can solve the problems of inability to use amphibious amphibious use, affecting the performance of amphibious hovercraft, and large weight of hovercraft, so as to improve the efficiency of research and development , The effect of reducing the number of on-site tests and shortening the development cycle
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[0024] The present invention will be further described in detail below in conjunction with the accompanying drawings, so that those skilled in the art can implement it with reference to the description.
[0025] Such as figure 1 As shown, the present invention provides a method for obtaining the wing installation angle of an amphibious hovercraft, comprising: Step 1, extracting and calculating the basic structural parameters of the amphibious hovercraft, specifically:
[0026] 1) Estimation of the total take-off weight of the amphibious hovercraft;
[0027] The main dimensions of the amphibious hovercraft are as follows:
[0028] Overall length: 760mm Overall width: 940mm
[0029] Wingspan: 350mm Apron volume: 0.42m2
[0030] The take-off weight of the amphibious hovercraft refers to the total weight at the beginning of the design-determined mission, where: W crew --The weight of the crew, the weight of three people is proposed to be used in this design; WF--the fuel weigh...
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