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Rather than having the wing next to the missiles in the same direction as the direction of travel, the missile is mounted slightly inclined to the resistance of the air by the law of reaction.
Rather than having the wing next to the missiles in the same direction as the direction of travel, the missile is mounted slightly inclined to the resistance of the air by the law of reaction.
The present invention relates to a method for reducing air resistance in flying objects such as a missile. According to the present invention, a wing of a missile is installed and mounted with a slight inclination to allow the missile to be advanced by a force received while the missile is flying. Accordingly, when the missile is advanced, the wing reduces air resistance.
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