Surface structure of missile

Abstract

The invention provides a surface structure of a missile, comprising nearly-bowl-shaped round pits, and the round pits are uniformly distributed on the surface of the missile, equal in size, and have a certain depth. Compared with a design that the surface of the existing missile is smooth, the surface structure disclosed by the invention can reduce the viscous effect of air on the surface of the missile, and reduce the air resistance of the missile in the process of flight, thereby speeding up the flight, and increasing the flight distance.

Description

technical field [0001] The invention relates to a missile surface structure. Background technique [0002] At present, the surface of the missile is designed to be smooth. When the missile is flying, the air forms a viscous effect on the surface of the missile, and the air resistance is large, which affects the flight speed and distance. Contents of the invention [0003] In order to overcome the above-mentioned deficiencies in the prior art, the present invention provides a surface structure of a missile, which includes uniformly distributed, equal in size, certain depth, and nearly bowl-shaped circular pits on the surface of the missile. Compared with the smooth surface design of the existing missile , the invention can reduce the air resistance when the missile is flying, accelerate the flying speed and increase the flying distance. Description of drawings [0004] attached figure 1 is a schematic diagram of the surface structure of the missile of the present invent...

AI Technical Summary

Problems solved by technology

[0002] At present, the surface of the missile is designed to be smooth. When the missile is flying, the air forms a viscous effect on the surface of the missile. The air resistance is large, which affects the flight speed and distance.

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