Rescue line-throwers: mathematical modeling and experimental researches

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The mathematical model of a line-thrower during the shot is considered. The shell with the line is the body with the variable mass. The Lagrange equations are derived and solved numerically. The results of the experimental studies are shown as the dependences of pressure obtained from the sensors of the laboratory test rig.

Pneumatic line-thrower, lagrange equations, computer mathematics, shot, test rig

Короткий адрес: https://sciup.org/148204366

IDR: 148204366

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