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yulyashka [42]
2 years ago
14

A block of mass M rests on a block of mass M1 = 5.00 kg which is on a tabletop. A light string passes over a frictionless peg an

d connects the blocks. The coefficient of kinetic friction μk at both surfaces equals 0.330. A force of F = 56.0 N pulls the upper block to the left and the lower block to the right. The blocks are moving at a constant speed.
Required:
Determine the mass of the upper block.
Engineering
1 answer:
MissTica2 years ago
4 0

Answer:

The mass of the upper block M = 4.12 kg

Explanation:

From the given information:

The upper block formula can be computed as :

F = T + F_{f1}

F - T - F_{f1} =0

where;

F_{f1} = \mu Mg

F - T - \mu Mg=0  ---- (1)

The lower block formula is as follows:

T - F_{f1} -F_{f2}  = 0

T - \mu Mg - \mu (M_1+M)g= 0

T = \mu Mg - \mu (M_1+M)g --- (2)

Equating equation (1) and  (2) together, we have:

F - \mu Mg - \mu Mg - \mu (M_1 + M) g = 0

56 - 3 Mg - \mu M_1g= 0

M = \dfrac{56 - \mu M_1 g}{3 \mu g}

M = \dfrac{56 - (0.330)(5)(9.8)}{3 (0.330) (9.8)}

M = \dfrac{56 - 16.17}{9.702}

M = \dfrac{39.83}{9.702}

M = 4.12 kg

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A piece of corroded steel plate was found in a submerged ocean vessel. It was estimated that the original area of the plate was
shepuryov [24]

Answer:

Time of submersion in years = 7.71 years

Explanation:

Area of plate (A)= 16in²

Mass corroded away = Weight Loss (W) = 3.2 kg = 3.2 x 106

Corrosion Penetration Rate (CPR) = 200mpy

Density of steel (D) = 7.9g/cm³

Constant = 534

The expression for the corrosion penetration rate is

Corrosion Penetration Rate = Constant x Total Weight Loss/Time taken for Weight Loss x Exposed Surface Area x Density of the Metal

Re- arrange the equation for time taken

T = k x W/ A x CPR x D

T = (534 x 3.2 x 106)/(16 x 7.9 x 200)

T = 67594.93 hours

Convert hours into years by

T = 67594.93 x (1year/365 days x 24 hours x 1 day)

T = 7.71 years

3 0
3 years ago
A three-phase line has an impedance of 0.4 j2.7 ohms per phase. The line feeds two balanced three-phase loads that are connected
Viktor [21]

Answer:

a. The magnitude of the line source voltage is

Vs = 4160 V

b. Total real and reactive power loss in the line is

Ploss = 12 kW

Qloss = j81 kvar

Sloss = 12 + j81 kVA

c. Real power and reactive power supplied at the sending end of the line

Ss = 540.046 + j476.95 kVA

Ps = 540.046 kW

Qs = j476.95 kvar

Explanation:

a. The magnitude of the line voltage at the source end of the line.

The voltage at the source end of the line is given by

Vs = Vload + (Total current×Zline)

Complex power of first load:

S₁ = 560.1 < cos⁻¹(0.707)

S₁ = 560.1 < 45° kVA

Complex power of second load:

S₂ = P₂×1 (unity power factor)

S₂ = 132×1

S₂ = 132 kVA

S₂ = 132 < cos⁻¹(1)

S₂ = 132 < 0° kVA

Total Complex power of load is

S = S₁ + S₂

S = 560.1 < 45° + 132 < 0°

S = 660 < 36.87° kVA

Total current is

I = S*/(3×Vload)   ( * represents conjugate)

The phase voltage of load is

Vload = 3810.5/√3

Vload = 2200 V

I = 660 < -36.87°/(3×2200)

I = 100 < -36.87° A

The phase source voltage is

Vs = Vload + (Total current×Zline)

Vs = 2200 + (100 < -36.87°)×(0.4 + j2.7)

Vs = 2401.7 < 4.58° V

The magnitude of the line source voltage is

Vs = 2401.7×√3

Vs = 4160 V

b. Total real and reactive power loss in the line.

The 3-phase real power loss is given by

Ploss = 3×R×I²

Where R is the resistance of the line.

Ploss = 3×0.4×100²

Ploss = 12000 W

Ploss = 12 kW

The 3-phase reactive power loss is given by

Qloss = 3×X×I²

Where X is the reactance of the line.

Qloss = 3×j2.7×100²

Qloss = j81000 var

Qloss = j81 kvar

Sloss = Ploss + Qloss

Sloss = 12 + j81 kVA

c. Real power and reactive power supplied at the sending end of the line

The complex power at sending end of the line is

Ss = 3×Vs×I*

Ss = 3×(2401.7 < 4.58)×(100 < 36.87°)

Ss = 540.046 + j476.95 kVA

So the sending end real power is

Ps = 540.046 kW

So the sending end reactive power is

Qs = j476.95 kvar

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3 years ago
1. Which of these is NOT a common type of Camber/Caster adjuster?
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Answer: I'm pretty sure Slots is the Answer

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The outer surface of a spacecraft in space has an emissivity of 0.6 and an absorptivity of 0.2 for solar radiation. If solar rad
garik1379 [7]

Answer:

Explanation:

Given

emmisivity of spacecraft \epsilon =0.6

absorptivity \alpha =0.2

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heat Absorbed by  spacecraft is

Q_{absorbed}=\alpha A_sq_{rad}

where A_s=Surface area of Sphere

Q_{absorbed}=0.2\times A_s\times 2100

Q_{absorbed}=420A_s

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When the radiation emitted equals to the solar energy absorbed

Q_{absorbed}=Q

420A_s=\epsilon \sigma A_sT^4

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6 0
3 years ago
Hard woods and tight curves should be cut using what blade speeds.
erica [24]

Answer:

slower

Explanation:

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4 0
3 years ago
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