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azamat
3 years ago
7

A rotator has a weight of 100lb with a centroidal radius of gyration of 9 in. Determine the moment of inertia about the center o

f gravity for the rotator.
Engineering
1 answer:
Ronch [10]3 years ago
8 0

Answer:

8100 lbin²

Explanation:

Moment or inertia is expressed using the formula

I = mr²

M is the mass of the body

r is the radius of gyration

Given

W = 100lb

r = 9in

Required

Moment of inertia

I = Wr²

I = 100(9)²

I = 100×81

I = 8100lbin²

Hence the moment of inertia about the center of gravity for the rotator is

8100 lbin²

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(a) Sabbir usually (sit)______ in the front bench.
klasskru [66]

Answer:

a)sits

b)is shining

d)have been living

Explanation:

5 0
3 years ago
The propeller shaft of the submarine experiences both torsional and axial loads. Draw Mohr's Circle for a stress element on the
Alina [70]

Answer: Attached below is the missing detail and Mohr's circle.

i) б1 =  9.6 Ksi

б2 = -10.7 ksi

ii) 10.2 Ksi

iii)  -0.51Ksi

Explanation:

First step :

direct compressive stress on shaft

бd = P / π/4 * d^2

      = -20 / 0.785 * 5^2  = -1.09 Ksi

shear stress at the outer surface due to torsion

ζ = 16*T / πd^3

  = (16 * 250 ) / π * 5^3  = 010.19 Ksi

<u>Calculate the Principal stress, maximum in-plane shear stress and average normal stress</u>

Using Mohr's circle ( attached below )

<u>i) principal stresses:</u>

б1 = 4.8 cm * 2 = 9.6 Ksi

б2 = -5.35 cm * 2 = -10.7 ksi

<u>ii) maximum in-plane shear stress</u>

ζ  = radius of Mohr's circle

   = 5.1 cm = 10.2 Ksi   ( Given that ; 1 cm = 2Ksi )

<u>iii) average normal stress</u>

 = 9.6 + ( - 10.7 ) / 2

  = -0.51Ksi

8 0
3 years ago
When the rod is circular, radial lines remain straight and sections perpendicular to the axis do not warp. In this case, the str
Murljashka [212]

The question is incomplete. The complete question is :

The solid rod shown is fixed to a wall, and a torque T = 85N?m is applied to the end of the rod. The diameter of the rod is 46mm .

When the rod is circular, radial lines remain straight and sections perpendicular to the axis do not warp. In this case, the strains vary linearly along radial lines. Within the proportional limit, the stress also varies linearly along radial lines. If point A is located 12 mm from the center of the rod, what is the magnitude of the shear stress at that point?

Solution :

Given data :

Diameter of the rod : 46 mm

Torque, T = 85 Nm

The polar moment of inertia of the shaft is given by :

$J=\frac{\pi}{32}d^4$

$J=\frac{\pi}{32}\times (46)^4$

J = 207.6 mm^4

So the shear stress at point  A is :

$\tau_A =\frac{Tc_A}{J}$

$\tau_A =\frac{85 \times 10^3\times 12 }{207.6}$

$\tau_A = 4913.29 \ MPa$

Therefore, the magnitude of the shear stress at point A is 4913.29 MPa.

3 0
3 years ago
Fatigue failure occurs under the condition of (a) High elastic stress (b) High corrosivity (c) High stress fluctuations (d) High
Harlamova29_29 [7]

Answer:

Fatigue occurs under conditions of high elastic stress, high stress fluctuations and high rate of loading

Explanation:

 According to many definition of fatigue failure the fatigue occurs when in an especifyc point of the object there is involved many forces and tensions.

 That tensions needs to be big in magnitud, de variations of the efforts it has to be with a lot of amplitude and the loading in the object it has to be with a lot of number of cycles.

 If in the all of these three conditions are present the fatigue failure it would appear.

8 0
4 years ago
Natural gas at and standard atmospheric pressure of 14.7 psi (abs) is compressed isentropically to a new absolute pressure of 70
padilas [110]

Complete question:

Natural gas at 70 ⁰F and standard atmospheric pressure of 14.7 psi (abs) is compressed isentropically to a new absolute pressure of 70 psi.  Determine the final density and temperature of the gas.

Answer:

The final density of the natural gas is 0.004243 slugs/ft³ and

The final temperature of the natural gas is 306.6 ⁰F

Explanation:

For Ideal gas: P = ρRT

R  is ideal gas constant =  3.099 x 10³  ft lb / slug⁰R

T₁ is initial temperature = 70 ⁰F = (70+460)⁰R = 530⁰R

P₁ is intial pressure of the gas = 14.7 psi = (14.7 lb/in² X 144 in²/ft²) = 2116.8 lb/ft²

From the ideal gas equation, we calculate initial density of the natural gas:

ρ₁ = P/RT ⇒ 2116.8/(3.099 x 10³ X 530) = 0.001289 slugs/ft³

For isentropic process:

\frac{P}{\rho^K} = Constant

where  K  is the ratio of specific heats for natural gas; K  =  1.31, Therefore

\frac{P_1}{\rho_1^{K}} = \frac{P_2}{\rho_2^{K}} ,\rho_2^K = (\frac{P_2}{P_1})\rho_1^K ,  \rho_2 = (\frac{P_2}{P_1})^\frac{1}{K}  \rho_1

\rho_2 = (\frac{70}{14.7})^\frac{1}{1.31} (0.001289) = (4.7619)^{0.76336}(0.001289) = 0.004243 slugs/ft³

Final density; ρ₂ = 4.243 X10⁻³ slugs/ft³

From ideal gas equation; P = ρRT

P₂ = ρ₂RT₂

T₂ = P₂/ρ₂R

P₂ (lb/ft²) =  (70 lb/in²)( 144 in²/ft²) = 10080 lb/ft²

T₂ = 10080/(0.004243 X 3099)

T₂ = 766.6⁰R

Final Temperature; T₂ = (766.6-460)⁰F = 306.6⁰F

7 0
3 years ago
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