Answer:
30.25 in Hg will be equal to 14.855 psi
Explanation:
We have given 30.25 Hg pressure
We have to convert the pressure of 30.25 Hg into psi
We know that 1 inch of Hg = 0.4911 psi
So to convert 30.25 inch Hg in psi we have to multiply with 0.4911
We have to convert 30.25 in Hg
So [tex]30.25inHg=30.25\times 0.4911=14.855775psi[/tex]
So 30.25 in Hg will be equal to 14.855 psi
2–25 Consider a medium in which the heat conduction equation is given in its simplest form as
d^2T/dx^2 + d^2T/dy^2 = 1/a dT/dt
(a) Is heat transfer steady or transient?
(b) Is heat transfer one-, two-, or three-dimensional?
(c) Is there heat generation in the medium?
(d) Is the thermal conductivity of the medium constant or variable?
Answer:
d) Is the thermal conductivity of the medium constant or variable.
Explanation:
As we know that
Heat equation with heat generation at unsteady state and with constant thermal conductivity given as
[tex]\dfrac{d^2T}{dx^2}+\dfrac{d^2T}{dy^2}+\dfrac{d^2T}{dz^2}+\dfrac{\dot{q}_g}{K}=\dfrac{1}{\alpha }\dfrac{dT}{dt}[/tex]
With out heat generation
[tex]\dfrac{d^2T}{dx^2}+\dfrac{d^2T}{dy^2}+\dfrac{d^2T}{dz^2}=\dfrac{1}{\alpha }\dfrac{dT}{dt}[/tex]
In 2 -D with out heat generation with constant thermal conductivity
[tex]\dfrac{d^2T}{dx^2}+\dfrac{d^2T}{dy^2}=\dfrac{1}{\alpha }\dfrac{dT}{dt}[/tex]
Given equation
[tex]\dfrac{d^2T}{dx^2}+\dfrac{d^2T}{dy^2}=\dfrac{1}{a }\dfrac{dT}{dt}[/tex]
So we can say that this is the case of with out heat generation ,unsteady state and with constant thermal conductivity.
So the option d is correct.
d) Is the thermal conductivity of the medium constant or variable.
A 1-mm-diameter methanol droplet takes 1 min for complete evaporation at atmospheric condition. What will be the time taken for a 1µm-diameter methanol droplet for complete evaporation at same conditions based on the scaling analysis?
Answer:
Time taken by the [tex]1\mu m[/tex] diameter droplet is 60 ns
Solution:
As per the question:
Diameter of the droplet, d = 1 mm = 0.001 m
Radius of the droplet, R = 0.0005 m
Time taken for complete evaporation, t = 1 min = 60 s
Diameter of the smaller droplet, d' = [tex]1\times 10^{- 6} m[/tex]
Diameter of the smaller droplet, R' = [tex]0.5\times 10^{- 6} m[/tex]
Now,
Volume of the droplet, V = [tex]\frac{4}{3}\pi R^{3}[/tex]
Volume of the smaller droplet, V' = [tex]\frac{4}{3}\pi R'^{3}[/tex]
Volume of the droplet ∝ Time taken for complete evaporation
Thus
[tex]\frac{V}{V'} = \frac{t}{t'}[/tex]
where
t' = taken taken by smaller droplet
[tex]\frac{\frac{4}{3}\pi R^{3}}{\frac{4}{3}\pi R'^{3}} = \frac{60}{t'}[/tex]
[tex]\frac{\frac{4}{3}\pi 0.0005^{3}}{\frac{4}{3}\pi (0.5\times 10^{- 6})^{3}} = \frac{60}{t'}[/tex]
t' = [tex]60\times 10^{- 9} s = 60 ns[/tex]
Heating of Oil by Air. A flow of 2200 lbm/h of hydrocarbon oil at 100°F enters a heat exchanger, where it is heated to 150°F by hot air. The hot air enters at 300°F and is to leave at 200°F. Calculate the total lb mol air/h needed. The mean heat capacity of the oil is 0.45 btu/lbm · °F.
Answer:
2062 lbm/h
Explanation:
The air will lose heat and the oil will gain heat.
These heats will be equal in magnitude.
qo = -qa
They will be of different signs because one is entering iits system and the other is exiting.
The heat exchanged by oil is:
qo = Gp * Cpo * (tof - toi)
The heat exchanged by air is:
qa = Ga * Cpa * (taf - tai)
The specific heat capacity of air at constant pressure is:
Cpa = 0.24 BTU/(lbm*F)
Therefore:
Gp * Cpo * (tof - toi) = Ga * Cpa * (taf - tai)
Ga = (Gp * Cpo * (tof - toi)) / (Cpa * (taf - tai))
Ga = (2200 * 0.45 * (150 - 100)) / (0.24 * (300 - 200)) = 2062 lbm/h
To calculate the total lb mol air/h needed to heat the hydrocarbon oil, we can use the principle of heat transfer. First, calculate the heat transfer between the hot air and the oil using the formula Q = mcΔT. Finally, divide the heat transfer by the heat capacity of air to find the total lb mol air/h needed.
Explanation:To calculate the total lb mol air/h needed to heat the hydrocarbon oil, we can use the principle of heat transfer. First, we need to calculate the heat transfer between the hot air and the oil using the formula Q = mcΔT, where Q is the heat transfer, m is the mass, c is the specific heat, and ΔT is the temperature difference. We know that the heat exchanger transfers 2200 lbm/h of oil from 100°F to 150°F, so the total heat transfer is Q = 2200 lbm/h * (150°F - 100°F) * 0.45 btu/lbm • °F. Next, we can calculate the lb mol of air needed by dividing the heat transfer by the heat capacity of air, which is 0.24 btu/lbm • °F. Therefore, the total lb mol air/h needed is Q / (0.24 btu/lbm • °F).
Give a reason why fighter aircraft use mid-wing design.
Explanation:
Mid-wing configuration places wings exactly at midline of airplane which means at half of height of fuselage. These airplanes are well balanced and also they have a large control surface area.It is the best option aerodynamically as these planes are streamlined much more and also has low interference drag as compared to the high and the low wing configurations.
The mid-wing has almost neutral roll stability that is further good from prespective of the combat as well as the aerobatic aircraft as mid-wing allows for performance of the rapid roll maneuvers with the minimum yaw coupling.
The Viscosity of Fluid: a)- resistance to flow b)- a measure of internal shear c)- depends upon shear forces and velocity profile d)- answers 1 and 3
Answer:
a)Resistance to flow
Explanation:
Viscosity of fluid:
Resistance to flow is called as viscosity of fluid.It is also know as fluid friction.It try to stop the flow of fluid.Viscosity of fluid is a property of fluid and it does mot depends on type of flow .
If fluid viscosity is high it means that it have very low flow ability.And opposite to viscosity is called fluidity.If fluidity is high then it means that it have low viscosity.
Viscosity are of two type
1.Dynamic viscosity
2.Kinematic viscosity
If the shearing stress is linearly related to the rate of shearing strain for a fluid, it is a_____ fluid. What are other types of fluids and how does their rate of shearing strain relate to shearing stress?
Answer:
If the shearing stress is linearly related to shearing strain then the fluid is called as Newtonian fluid.
Explanation:
The other types of fluids are:
1) Non-Newtonian fluids which are further classified as
a) Thixotropic Fluid: Viscosity decreases with shearing stress over time.
b) Rehopactic Fluid: Viscosity increases with shearing stress over time.
c) Dilatant Fluid: Apparent viscosity increases with increase in stress.
d) Pseudoplastic: Apparent viscosity decreases with increase in stress.
Answer:
If the shearing stress is linearly related to shearing strain then the fluid is called as Newtonian fluid.
Explanation:
Why is the process for making flat glass called the float process?
Explanation:
Step1
Float glass is the process of glass manufacturing on the flat surface of metal like tin. In this method molten glass is allowed to float on the surface of metal.
Step2
Float glass gives the uniform and flat surface of glass product. The thickness of the glass produced is uniform throughout. This process of glass making is very cheap and has negligible distortion. Flat glass process is called the float process because of producing high quality flat surface.
What is the maximum % carbon for structural steel?
Answer:
The large percentage of steel includes less than 0.35% carbon
Explanation:
Carbon is perhaps the most important business alloy of steel. Raising carbon material boosts strength and hardness and enhances toughness. However, carbon often increases brittleness.
The large percentage of steel includes less than 0.35% carbon. Any steel with a carbon content range of 0.35% to 1.86% can be considered as hardened.
The temperature at the outlet of the turbocharger turbine is 260°C, with an exhaust flow rate of 2 kg/min. Estimate the drop in temperature across the turbine, given that the turbine output power is 1kW. Assume exhaust gas to have a specific heat of 1.05 kJ/kg.K, and an ambient temperature of 25°C
Answer:
[tex]\Delta T = 28.57°C[/tex]
Explanation:
given data:
temperature at outlet of turbine = 260°C
Flow rate = 2 kg/min = 0.033 kg/s
output power = 1 kW
specific heat = 1.05 kJ/kg.K
We know that power generated by turbine is equal to change in enthalpy
[tex]W = h_2 - h_1[/tex]
[tex]= mCp(\Delta T)[/tex]
[tex]1*10^3 = 0.0333*1.05*10^3 * \Delta T[/tex]
[tex]\Delta T = \frac{10^3}{0.033*1.05*10^3}[/tex]
[tex]\Delta T = 28.57°C[/tex]
A body is moving with simple harmonic motion. It's velocity is recorded as being 3.5m/s when it is at 150mm from the mid-position and 2.5m/s when 225mm from mid-position. Find : i) It's max amplitude ii) Max acceleration iii) The periodic time iv) The frequency of oscillation.
Answer:
1) A=282.6 mm
2)[tex]a_{max}=60.35\ m/s^2[/tex]
3)T=0.42 sec
4)f= 2.24 Hz
Explanation:
Given that
V=3.5 m/s at x=150 mm ------------1
V=2.5 m/s at x=225 mm ------------2
Where x measured from mid position.
We know that velocity in simple harmonic given as
[tex]V=\omega \sqrt{A^2-x^2}[/tex]
Where A is the amplitude and ω is the natural frequency of simple harmonic motion.
From equation 1 and 2
[tex]3.5=\omega \sqrt{A^2-0.15^2}[/tex] ------3
[tex]2.5=\omega \sqrt{A^2-0.225^2}[/tex] --------4
Now by dividing equation 3 by 4
[tex]\dfrac{3.5}{2.5}=\dfrac {\sqrt{A^2-0.15^2}}{\sqrt{A^2-0.225^2}}[/tex]
[tex]1.96=\dfrac {{A^2-0.15^2}}{{A^2-0.225^2}}[/tex]
So A=0.2826 m
A=282.6 mm
Now by putting the values of A in the equation 3
[tex]3.5=\omega \sqrt{A^2-0.15^2}[/tex]
[tex]3.5=\omega \sqrt{0.2826^2-0.15^2}[/tex]
ω=14.609 rad/s
Frequency
ω= 2πf
14.609= 2 x π x f
f= 2.24 Hz
Maximum acceleration
[tex]a_{max}=\omega ^2A[/tex]
[tex]a_{max}=14.61 ^2\times 0.2826\ m/s^2[/tex]
[tex]a_{max}=60.35\ m/s^2[/tex]
Time period T
[tex]T=\dfrac{2\pi}{\omega}[/tex]
[tex]T=\dfrac{2\pi}{14.609}[/tex]
T=0.42 sec
To unload a bound stack of plywood from a truck, the driver first tilts the bed of the truck and then accelerates from rest. Knowing that the coefficients of friction between the bottom sheet of plywood and the bed are fJK = 0.40 and fik = 0.30, determine (a) the smallest acceleration of the truck which will cause the stack of plywood to slide, (b) the acceleration of the truck which causes corner A of the stack of plywood to reach the end of the bed in 0.4 s.
Answer:
a) The truck must have an acceleration of at least 3.92 * cos(θ)^2 for the stack to start sliding.
b) a = 2.94 * cos(θ)^2 + 0.32 * L * cos(θ)
Explanation:
The stack of plywood has a certain mass. The weight will depend on that mass.
w = m * g
There will be a normal reaction between the stack and the bed of the truck, this will be:
nr = -m * g * cos(θ)
Being θ the tilt angle of the bed.
The static friction force will be:
ffs = - m * g * cos(θ) * fJK
The dynamic friction force will be:
ffd = - m * g * cos(θ) * fik
These forces would produce accelerations
affs = -g * cos(θ) * fJK
affd = -g * cos(θ) * fik
affs = -9.81 * cos(θ) * 0.4 = -3.92 * cos(θ)
affd = -9.81 * cos(θ) * 0.3 = -2.94 * cos(θ)
These accelerations oppose to movement and must be overcome by another acceleration to move the stack.
The acceleration of the truck is horizontal, the horizontal component of these friction forces is:
affs = -3.92 * cos(θ)^2
affd = -2.94 * cos(θ)^2
The truck must have an acceleration of at least 3.92 * cos(θ)^2 for the stack to start sliding.
Assuming the bed has a lenght L.
The horizontal movement will be over a distance cos(θ) * L because L is tilted.
Movement under constant acceleration:
X(t) = X0 + V0 * t + 1/2 * a * t^2
In this case X0 = 0, V0 = 0, and a will be the sum of the friction force minus the acceleration of the truck.
If we set the frame of reference with the origin on the initial position of the stack and the positive X axis pointing backwards, the acceleration of the truck will now be negative and the dynamic friction acceleration positive.
L * cos(θ) = 1/2 * (2.94 * cos(θ)^2 - a) * 0.4^2
2.94 * cos(θ)^2 - a = 2 * 0.16 * L * cos(θ)
a = 2.94 * cos(θ)^2 + 0.32 * L * cos(θ)
True False. First angle projection type used in United states.
Answer:
FALSE.
Explanation:
the correct answer is FALSE.
Projection is the process of representing the 3 D object on the flat surface.
there are four ways of representing the projection
1) First angle projection
2) second angle projection
3) third angle projection
4) fourth angle projection.
Generally, people prefer First and third angle projection because there is no overlapping of the projection take place.
In USA people uses the third angle of projection.
Two wafer sizes are to be compared: a 156-mm wafer with a processable area = 150mm diameter circle and a 312-mm wafer with a processable area = 300mm diameter circle. The IC chips in both cases are square with 10 mm on a side? Assume the cut lines (streets) between chips are of negligible width. What is the percent increase in (a) Wafer diameter, (b) processable wafer area, and (c) number of chips for the larger wafer size?
Answer:
a) 100%
b) 300%
c) 301 %
Explanation:
The first wafer has a diameter of 150 mm.
The second wafer has a diameter of 300 mm.
The second wafer has an increase in diameter respect of the first of:
((300 / 150) - 1) * 100 = 100%
The first wafers has a processable area of:
A1 = π/4 * D1^2
The scond wafer has a processable area of:
A2 = π/4 * D2^2
The seconf wafer has a increase in area respect of the first of:
(A2/A1 * - 1) * 100
((π/4 * D2^2) / (π/4 * D1^2) - 1) * 100
((D2^2) / (D1^2) - 1) * 100
((300^2) / (150^2) - 1) * 100 = 300%
The area of a chip is
Ac = Lc^2
So the chips that can be made from the first wafer are:
C1 = A1 / Ac
C1 = (π/4 * D1^2) / Lc^2
C1 = (π/4 * 150^2) / 10^2 = 176.7
Rounded down to 176
The chips that can be made from the second wafer are:
C2 = A2 / Ac
C2 = (π/4 * D2^2) / Lc^2
C2 = (π/4 * 300^2) / 10^2 = 706.8
Rounded down to 706
The second wafer has an increase of chips that can be made from it respect of the first wafer of:
(C2 / C1 - 1) * 100
(706 / 176 - 1) *100 = 301%
A car is traveling at 36 km/h on an acceleration lane to a freeway. What acceleration is required to obtain a speed of 72 km/h in a distance of 100m? What time is required to travel this distance?
First, write down the information given and the change units if necessary (we must have similar units to operate on).
Initial speed, u = 36 km/h = 10 m/s
Final speed, v = 72 km/h = 20 m/s
Distance, s = 100 m
We know that
[tex] {v}^{2} - {u}^{2} = 2as \\ {20}^{2} - {10}^{2} = 2 \times a \times 100 \\ 400 - 100 = 200 \times a \\ a = \frac{300}{200 } = \frac{3}{2} \: m {s}^{ - 2} [/tex]
Now, we substitute v, u, and a in the formula
[tex]v = u + at \\ 20 = 10 + \frac{3}{2} t \\ \frac{3}{2} t = 10 \\ 3t = 20 \\ t = \frac{20}{3} = 6.67 \: seconds[/tex]
Please mark Brainliest if this helps!
Air enters a 34 kW electrical heater at a rate of 0.8 kg/s with negligible velocity and a temperature of 60 °C. The air is discharged at a height 50 m above the inlet at a temper-ature of 200 °C and a velocity of 50 m / s. What is the work done in the heater?
Answer:
79 kW.
Explanation:
The equation for enthalpy is:
H2 = H1 + Q - L
Enthalpy is defined as:
H = G*(Cv*T + p*v)
This is specific volume.
The gas state equation is:
p*v = R*T (with specific volume)
The specific gas constant for air is:
287 K/(kg*K)
Then:
T1 = 60 + 273 = 333 K
T2 = 200 + 273 = 473 K
p1*v1 = 287 * 333 = 95.6 kJ/kg
p2*v2 = 287 * 473 = 135.7 kJ/kg
The Cv for air is:
Cv = 720 J/(kg*K)
So the enthalpies are:
H1 = 0.8*(0.72 * 333 + 95.6) = 268 kW
H2 = 0.8*(0.72 * 473 + 135.7) = 381 kW
Ang the heat is:
Q = 34 kW
Then:
H2 = H1 + Q - L
381 = 268 + 34 - L
L = 268 + 34 - 381 = -79 kW
This is the work from the point of view of the air, that's why it is negative.
From the point of view of the machine it is positive.
A person, 175 lbm, wants to fly (hoover) on a 4 lbm skateboard of size 2 ft by 0.8 ft. How large a gauge pressure under the board is needed?
Answer:
[tex]p = 15260.643 \ lbf/ft^2[/tex]
Explanation:
person weight is 175 lbm
weight of stake board 4lbm
size of stakeboard = 2ft by 0.8 ft
area of stakeboard is [tex]2*0.8 ft^2 = 1.6 ft^2[/tex]
gauge pressure is given as
[tex]p =\frac{ w_p+w_s}{A} g[/tex]
where is g is acceleration due to gravity = 32.17 ft/sec^2
puttng all value to get pressure value
[tex]= \frac{175 +4}{1.6}* 32.17[/tex]
[tex]p = 15260.643 \ lbf/ft^2[/tex]
The roof of a car in a parking lot absorbs a solar radiant flux of 800 W/m2, and the underside is perfectly insulated. The convection coefficient between the roof and the ambient air is 12 W/m2·K. (a) Neglecting radiation exchange with the surroundings, calculate the temperature of the roof under steady state conditions if the ambient air temperature is 20°C. (b) For the same ambient air temperature, calculate the temperature of the roof if its surface emissivity is 0.8.
The roof temperature is calculated to be 93°C without radiation or 86.67°C when accounting for radiation heat transfer with the surroundings.
Given: q = 800 W/m2 h = 12 W/m2∙K T∞ = 293 K
Convection heat transfer equation: q = hA(Ts - T∞)
Plug in values: 800 W/m2 = 12 W/m2∙K (Ts - 293 K)
Distribute the 12 W/m2∙K: 800 W/m2 = 12 W/m2∙K * Ts - 12 W/m2∙K * 293 K
Group the Ts terms: 800 W/m2 = 12 W/m2∙K * Ts - 3,516 W/m2
Add 3,516 W/m2 to both sides: 4,316 W/m2 = 12 W/m2∙K * Ts
Divide both sides by 12 W/m2∙K: Ts = 4,316 W/m2 / 12 W/m2∙K
Calculate:
Ts = 366 K = 93°C
(a) Without radiation: Heat transfer equation: q = hA(Ts - T∞)
Plug in values: 800 W/m2 = 12 W/m2∙K (Ts - 293 K) 800 = 12(Ts - 293) Ts = 800/12 + 293 Ts = 366 K = 93°C
(b) With radiation: Heat transfer equation:
q = hA(Ts - T∞) + εσA(Ts4 - Tsur4)
Given: T∞ = 293 K ε = 0.8
σ = 5.67x10-8 W/m2∙K4
Radiation heat transfer equation: q = εσA(Ts4 - Tsur4)
Assume: Tsur = T∞ = 293 K
Plug in values: q = 0.8 * 5.67x10-8 * A * (Ts4 - (293)4)
(293)4 evaluation: (293)4 = 293 x 293 x 293 x 293 = 2.97 x 108
Plug this into equation:
q = 0.8 * 5.67x10-8 * A * (Ts4 - 2.97x108)
800 = 12(Ts - 293) + 0.8*5.67x10-8(Ts4 - 2.97x108)
Solve for Ts: Ts = 359.8 K = 86.67°C
Therefore, with radiation the roof temperature is 86.67°C.
Part A: The temperature of the roof under steady-state conditions without considering radiation exchange is 86.67°C.
Part B: The temperature of the roof under steady-state conditions considering radiation exchange with an emissivity of 0.8 is 81.17°C.
Part A: Neglecting Radiation Exchange
Step 1
Under steady-state conditions, the heat absorbed by the roof [tex](\( Q_{\text{absorbed}} \))[/tex] is equal to the heat lost through convection [tex](\( Q_{\text{convection}} \))[/tex].
Given:
- Solar radiant flux, [tex]\( q_{\text{solar}} = 800 \, \text{W/m}^2 \)[/tex]
- Convection coefficient, [tex]\( h = 12 \, \text{W/m}^2 \cdot \text{K} \)[/tex]
- Ambient air temperature, [tex]\( T_{\infty} = 20^\circ \text{C} \)[/tex]
The absorbed heat:
[tex]\[ Q_{\text{absorbed}} = q_{\text{solar}} \][/tex]
The heat loss by convection:
[tex]\[ Q_{\text{convection}} = h (T_s - T_{\infty}) \][/tex]
At steady state:
[tex]\[ q_{\text{solar}} = h (T_s - T_{\infty}) \][/tex]
Step 2
Solving for the surface temperature [tex]\( T_s \)[/tex]:
[tex]\[ 800 = 12 (T_s - 20) \][/tex]
[tex]\[ T_s - 20 = \frac{800}{12} \][/tex]
[tex]\[ T_s - 20 = 66.67 \][/tex]
[tex]\[ T_s = 86.67^\circ \text{C} \][/tex]
So, the temperature of the roof under steady-state conditions without radiation exchange is 86.67°C.
Part B: Considering Radiation Exchange
Step 1
When considering radiation exchange, the roof loses heat through both convection and radiation. The net radiative heat loss is given by the Stefan-Boltzmann law.
Given:
- Emissivity, [tex]\( \varepsilon = 0.8 \)[/tex]
- Stefan-Boltzmann constant, [tex]\( \sigma = 5.67 \times 10^{-8} \, \text{W/m}^2 \cdot \text{K}^4 \)[/tex]
The total heat loss (convection + radiation):
[tex]\[ Q_{\text{total}} = Q_{\text{convection}} + Q_{\text{radiation}} \][/tex]
For convection:
[tex]\[ Q_{\text{convection}} = h (T_s - T_{\infty}) \][/tex]
For radiation:
[tex]\[ Q_{\text{radiation}} = \varepsilon \sigma (T_s^4 - T_{\infty}^4) \][/tex]
At steady state:
[tex]\[ q_{\text{solar}} = h (T_s - 20) + \varepsilon \sigma (T_s^4 - 293.15^4) \][/tex]
[tex]\[ 800 = 12 (T_s - 20) + 0.8 \times 5.67 \times 10^{-8} (T_s^4 - 293.15^4) \][/tex]
Step 2
To simplify:
[tex]\[ 800 = 12 (T_s - 20) + 4.536 \times 10^{-8} (T_s^4 - 293.15^4) \][/tex]
This equation is nonlinear and needs to be solved iteratively. Let's outline the steps to solve it without detailed iteration steps:
1. Initial Guess: Start with an initial guess for [tex]\( T_s \)[/tex].
2. Iteration: Adjust [tex]\( T_s \)[/tex] until both sides of the equation are equal.
Through iteration or numerical methods, we find:
[tex]\[ T_s \approx 81.17^\circ \text{C} \][/tex]
In summary, the temperature of the roof is 86.67°C without considering radiation, and it drops to approximately 81.17°C when radiation exchange is taken into account.
A rigid, sealed cylinder initially contains 100 lbm of water at 70 °F and atmospheric pressure. Determine: a) the volume of the tank (ft3 ). Later, a pump is used to extract 10 lbm of water from the cylinder. The water remaining in the cylinder eventually reaches thermal equilibriu
Answer:
Determine A) The Volume Of The Tank (ft^3) Later A Pump Is Used To Extract ... A rigid, sealed cylinder initially contains 100 lbm of water at 70 degrees F and atmospheric pressure. ... Later a pump is used to extract 10 lbm of water from the cylinder. The water remaining in the cylinder eventually reaches thermal equilibrium ...
A 15,000lb freight car is pulled along a horizontal track.
Ifthe car starts from rest and attains a velocity of 40ft/s
aftertraveling a distance of 300ft.
determine the total work done on the car by the towing forcein
this distance if the rolling frictional force between the carand
the track is 80lb.
Answer:
12024000 lb*ft
Explanation:
The total work will be the sum of the energy consumed by friction plus the kinetic energy the car attained.
L = Ek + Lf
Lf = Ff * d
Ek = 1/2 * m * v^2
Therefore:
L = Ff * d + 1/2 * m * v^2
L = 80 * 300 + 1/2 * 15000 * 40^2 = 12024000 lb*ft
THe total work done on the car is of 12024000 lb*ft
An aircraft is in a steady level turn at a flight speed of 200 ft/s and a turn rate about the local vertical of 5 deg/s. Thrust from the engine is along the flight direction. Given the weight of the aircraft as 50,000 lb and L/D of 10, determine the lift, drag and thrust required for the given equilibrium flight. Assume g =32.2 ft/s^2
Answer:
L= 50000 lb
D = 5000 lb
Explanation:
To maintain a level flight the lift must equal the weight in magnitude.
We know the weight is of 50000 lb, so the lift must be the same.
L = W = 50000 lb
The L/D ratio is 10 so
10 = L/D
D = L/10
D = 50000/10 = 5000 lb
To maintain steady speed the thrust must equal the drag, so
T = D = 5000 lb
A piston-cylinder assembly contains a two-phase liquid-vapor mixture of H20 at 220 lbf/in^2 with a quality of 75%. The mixture is heated and expands at constant pressure until a final temperature of 475°F is reached. Determine the work for the process, in Btu per lb of H2O present.
To determine the work in a thermodynamic process of a two-phase liquid-vapor mixture of H2O, use the provided formula considering initial and final conditions, enabling calculation of the energy transferred.
Explanation:In this thermodynamic process, the work done can be calculated using the area under the constant pressure line on a P-v diagram. Given the initial and final conditions, the work for the process can be determined.
To calculate the work, use the formula: W = m*(P_final*V_final - P_initial*V_initial)/(1-q), where 'm' is the mass of the substance, 'P' is the pressure, 'V' is the specific volume, and 'q' is the quality of the mixture.
Substitute the values into the formula, convert units as necessary, and calculate the work to find the energy transferred during the process in Btu per lb of H2O present.
A water filled vertical u-tube manometer is used to measure pressure changes in a reaction vessel. Assuming that the change in height of the manometer can be measured to a precision of 1/16" of an inch, how accurately can pressure changes (in psi) be measured?
Answer:
The pressure will be measured to a precision of 0.073 psi.
Explanation:
Since the relation between the measurement of pressure and height is given by
[tex]dP=\rho gh[/tex]
For water we have
[tex]\rho _{water}=62.4lb/ft^3[/tex]
[tex]g=32.17ft/s^2[/tex]
Applying the given values we get
[tex]dP=62.4\times 32.17\times \frac{1}{16\times 12}=5.433lb/ft^2\\\\=\frac{10.455}{144}lb/in^2=0.073psi[/tex]
Find the difference between the first and third angle projection type.
Answer:
First angle projection
1.Object is between observer and plane of projection.
2.Projection of object take on first quadrant.
3.Plane of projection is assume non transparent.
Third angle projection:
1.Plane of projection is between observer and object.
2.Projection of object take on third quadrant.
3.Plane of projection is assume transparent.
A steam turbine has isentropic efficiency of 0.8. Isentropically, it is supposed to deliver work of 100 kW. What is the actual work delivered by the turbine? A heat pump has a COP of 2.2. It takes 5 kW electric power. What is the heat delivery rate to the room being heated in kW? Heat pump is used for winter heating of a room. A refrigerator takes 5 kW electric power. It extracts 3 kW of heat from the space being cooled a. What is the heat delivery rate to the surroundings in kW? b. What is the COP of the refrigerator?
Answer:
80 kW; 11 kW; 8 kW; 0.6
Explanation:
Part 1
Isentropic turbine efficiency:
[tex]\eta_t = \frac{\text{Real turbine work}}{\text{isentropic turbine work}} = \frac{W_{real}}{W_s} [/tex]
[tex]W_{real} = \eta_t*W_s [/tex]
[tex]W_{real} = 0.8*100 kW [/tex]
[tex]W_{real} = 80 kW [/tex]
Part 2
Coefficient of performance COP is defined by:
[tex]COP = \frac{Q_{out}}{W} [/tex]
[tex]Q_{out} = W*COP[/tex]
[tex]Q_{out} = 5 kW*2.2[/tex]
[tex]Q_{out} = 11 kW[/tex]
Part 3
(a)
Energy balance for a refrigeration cycle gives:
[tex]Q_{in} + W = Q_{out} [/tex]
[tex]3 kW + 5 kW = Q_{out} [/tex]
[tex]8 kW = Q_{out} [/tex]
(b)
[tex]COP = \frac{Q_{in}}{W} [/tex]
[tex]COP = \frac{3 kW}{5 kW} [/tex]
[tex]COP = 0.6 [/tex]
A bar of 75 mm diameter is reduced to 73mm by a cutting tool while cutting orthogonally. If the mean length of the cut chip is 73.5 mm, find the cutting ratio. If the rake angle is 15 deg, what is the shear angle?
The cutting ratio is 0.027, and the shear angle is 88.46 degrees.
The Breakdown
- Initial diameter of the bar: 75 mm
- Final diameter of the bar after cutting: 73 mm
- Mean length of the cut chip: 73.5 mm
- Rake angle: 15 degrees
Calculate the cutting ratio.
Cutting ratio = (Initial diameter - Final diameter) / Mean length of the cut chip
Cutting ratio = (75 mm - 73 mm) / 73.5 mm
Cutting ratio = 0.027
Calculate the shear angle.
The shear angle (φ) can be calculated using the following formula:
tan(φ) = (1 - cutting ratio) / (cutting ratio × cos(α))
Where:
α = Rake angle (in radians)
Substituting the given values:
α = 15 degrees = 15 × π/180 = 0.2618 radians
Cutting ratio = 0.027
tan(φ) = (1 - 0.027) / (0.027 × cos(0.2618))
φ = tan-¹(0.9730 / 0.0265)
φ = 88.46 degrees
Therefore, the cutting ratio is 0.027, and the shear angle is 88.46 degrees.
Dfine factor of safety and its significance
Explanation:
Step1
Factor of safety is the constant factor which is taken for the safe design of any product. It is the ratio of maximum stress induced in the material or the failure stress from tensile test to the allowable stress.
Step2
It is an important parameter for design of any component. This factor of safety is taken according to the type of material, environment condition, strength needed, type of component etc.
The expression for factor of safety is given as follows:
[tex]FOS=\frac{\sigma_{f}}{\sigma_{a}}[/tex]
Here, [tex]\sigma_{f}[/tex] is fracture stress and [tex]\sigma_{a}[/tex] is allowable stress.
What is the primary structural difference between cantilever wing and semi-cantilever wing?
Answer:
The main component of fixed wing aircraft
1.Wings
2.Fuselages
3.Landing gear
4.Stabilizers
5.Flight control surface
Cantilever wing:
A cantilever wing is directly attached to the fuselages and do not have any external support.
Semi cantilever wing:
A cantilever wing does not directly attached to the fuselages and have any external support.The external support may be one two.
An aluminum rod if 20 mm diameter iselongated 3.5 mm along its
longitudinal direction by a load of 25KN. If the modulus of
elasticity of aluminum is E = 70 GPa,determine the original length
of the bar.
Answer:
3.0772 m
Explanation:
Given:
Diameter of the aluminium rod, d = 20 mm = 0.02 m
Length of elongation, δL = 3.5 mm = 0.0035 m
Applied load, P = 25 KN = 25000 N
Modulus of elasticity, E = 70 GPa = 70 × 10⁹ N/m²
Now,
we have the relation
[tex]\delta L=\frac{\textup{PL}}{\textup{AE}}[/tex]
Now,
Where, A is the area of cross-section
A = [tex]\frac{\pi}{4}d^2[/tex]
or
A = [tex]\frac{\pi}{4}\times0.02^2[/tex]
or
A = 0.000314 m²
L is the length of the member
on substituting the respective values, we get
[tex]0.0035=\frac{25000\times L}{0.000314\times70\times10^9}[/tex]
or
L = 3.0772 m
In laminar now, fluid particles are constrained to motion in (parallel —perpendicular opposite) paths by the action of (temperature- viscosity —pressure).
Answer:
parallel ; Viscosity
Explanation:
Laminar is flow is the flow of fluid layer in which motion of the liquid particle is very slow and there is no intermixing of the layer of fluid takes place.
There no perpendicular movement of particles takes place, no eddies are formed or swirl of fluid.
so, the first option will be Parallel. Fluid particles flow parallel to each other in laminar flow.
This path of flow is by the action of Viscosity of the fluid.
Two streams of air enter a control volume: stream 1 enters at a rate of 0.05 kg / s at 300 kPa and 380 K, while stream 2 enters at 400 kPa and 300 K. Stream 3 leaves the control volume at 150 kPa and 270 K. The control volume does 3 kW of work on the surroundings while losing 5 kW of heat. Find the mass flow rate of stream 2. Neglect changes in kinetic and potential energy.
Answer:
0.08kg/s
Explanation:
For this problem you must use 2 equations, the first is the continuity equation that indicates that all the mass flows that enter is equal to those that leave the system, there you have the first equation.
The second equation is obtained using the first law of thermodynamics that indicates that all the energies that enter a system are the same that come out, you must take into account the heat flows, work and mass flows of each state, as well as their enthalpies found with the temperature.
finally you use the two previous equations to make a system and find the mass flows
I attached procedure