Solution D1-56 (Figure D1.5 condition 6 S.M. Targ 1989)

Solution to problem D1-56 (see Figure D1.5, condition 6, S.M. Targ, 1989).

Let us assume that a load D of mass m receives an initial velocity v0 at point A and moves along a curved pipe ABC located in a vertical plane. Pipe sections can be inclined or one of them can be horizontal and the other inclined (see Figures D1.0 - D1.9 and Table D1).

In section AB, in addition to the force of gravity, the load is acted upon by a constant force Q (its direction is shown in the figures) and a resistance force of the medium R, which depends on the speed v of the load and is directed against the movement. We can neglect the friction of the load on the pipe in section AB.

At point B, the load, without changing its speed, moves to the section BC of the pipe, where, in addition to the force of gravity, it is acted upon by the friction force (friction coefficient of the load on the pipe f = 0.2) and the variable force F, the projection of which Fx on the x axis given in the table.

Assuming that the load is a material point, and knowing the distance AB = l or the time t1 of movement of the load from point A to point B, it is necessary to find the law of movement of the load in the section BC, that is, x = f(t), where x = BD.

The digital goods store presents a solution to problem D1-56, which can be found in the textbook by S.M. Targa "Motion of ideal liquid and gas." The solution includes condition 6 with Figure D1.5, created in 1989.

The design of this product is made using beautiful html code, which allows you to conveniently view and study the material. By purchasing this solution, you receive a complete and understandable answer to problem D1-56, which can be useful for students and teachers studying physics.

The solution to problem D1-56 is a complete answer to the problem posed, described in condition 6 with Figure D1.5 from the textbook by S.M. Targa "Motion of Ideal Liquids and Gases" 1989 edition. The problem considers the movement of a load D with mass m, which receives an initial speed v0 at point A and moves along a curved pipe ABC located in a vertical plane.

In section AB, in addition to the force of gravity, the load is acted upon by a constant force Q and a resistance force of the medium R, which depends on the speed v of the load and is directed against the movement. The friction of the load on the pipe in section AB is not taken into account. At point B, the load passes to section BC of the pipe, where it is acted upon by a friction force (coefficient of friction of the load on the pipe f = 0.2) and a variable force F, the projection of which Fx on the x axis is given in the table.

Solving the problem allows us to find the law of movement of the load on the aircraft section, that is, x = f(t), where x = BD. The product design is made using beautiful html code, which makes it easy to view and study the material. The solution may be useful for students and teachers studying physics.

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Solution D1-56 is a problem involving the movement of a load of mass m along a curved pipe ABC located in a vertical plane. The load receives an initial speed v0 at point A and moves along the section AB, in which the load is acted upon by a constant force Q and a resistance force of the medium R, depending on the speed of the load. At point B, the load moves to section BC, where the load is acted upon by a frictional force and a variable force F, the projection of which Fx on the x axis is given in the table. The coefficient of friction of the load on the pipe f is 0.2.

It is necessary to find the law of cargo movement on the aircraft section, that is, the function x = f(t), where x is the distance between points B and D, and t is the time of cargo movement on the aircraft section.

To solve the problem, it is necessary to use Newton's laws and the equation of motion of a material point. In addition, it is necessary to take into account the dependence of the resistance force of the medium on the speed of the load and take into account the friction force and the variable force F in the aircraft section.

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