Questions
As temperature increases toward the critical temperature, the values of v_f and v_g become more far...

As temperature increases toward the critical temperature, the values of v_f and v_g become more far away from each other.

In: Mechanical Engineering

A motor apply power 10-hp split-phase motor speed at 1700 rpm is used to drive a...

A motor apply power 10-hp split-phase motor speed at 1700 rpm is used to drive a rotary pump, which operates 24 hours per day. An engineer has specified a 7-in small sheave, an 10-in large sheave, and three C112 belts. The service factor of 1.2 was augmented by 0.1 because of the continuous-duty requirement. Analyze the drive and estimate the belt life in passes and hours.

In: Mechanical Engineering

Given the “As Received” analysis of a coal:      Sulfur           = 1.52%                  Hydrogen&

Given the “As Received” analysis of a coal:

     Sulfur           = 1.52%                  Hydrogen      = 6.36%

     Carbon         = 79.56%                Nitrogen        = 1.42%

     Oxygen         = 5.02%                  Moisture       = 2.51%

     Ash              = 6.12%

Using the ASH AND MOISTURE FREE ANALYSIS OF THE COAL, calculate the following:

a) Theoretical O/F ratio

b) Actual A/F ratio at 20% excess air

c) Gravimetric Analysis of wet gas

d) Volumetric Analysis of dry gas

e) LHV of the fuel in kJ/kg

In: Mechanical Engineering

a viscous turbulent flow can be described by which equtions

a viscous turbulent flow can be described by which equtions

In: Mechanical Engineering

write the mathematical code in language fortran 77 about Linda Hanson palstic cryocooler refrigerator using r407c...

write the mathematical code in language fortran 77 about Linda Hanson palstic cryocooler refrigerator using r407c refrigerant with moving coil magnet compressor technology the compressor is used is scroll casing using r407c refrigerant hand blender ammonia and solid CO2

In: Mechanical Engineering

For a marine diesel engine application, a fluid-film journal bearing has a shaft diameter of 32...

For a marine diesel engine application, a fluid-film journal bearing has a shaft diameter of 32 mm and the length of the bearing is 24 mm. The bearing uses SAE grade 20 oil as lubricant and operates under a radial load. The inlet and outlet temperatures of oil are 50oC and 110oC respectively. It is assumed that because of the shearing action there is a uniformly distributed energy release in the lubricant that heats the lubricant film. During run-in operation, the film temperature can be approximated as the average of the inlet and outlet temperatures. Assuming reasonable design data, perform an overall design assessment for the following four cases:

Case 1: Applied load: 2.5 kN, Radial clearance: 0.04 mm, Shaft speed: 1800 rpm

Case 2: Applied load: 5.0 kN, Radial clearance: 0.04 mm, Shaft speed: 1800 rpm

Case 3: Applied load: 2.5 kN, Radial clearance: 0.04 mm, Shaft speed: 3600 rpm

Case 4: Applied load: 2.5 kN, Radial clearance: 0.02 mm, Shaft speed: 1800 rpm

a) Analyze and estimate the bearing design parameters such as, minimum film thickness, power loss, side flow, total flow and maximum film pressure for the above four cases.

b) Which parameter is most influential for economical running of the bearing ? Justify with reasons.

c) Which parameter is most influential for safe running of the bearing ? Justify with reasons.

d) Compare and discuss the results for the above four cases.

In: Mechanical Engineering

In view of the product life cycle, consider the progression that the EV (electric vehicle) industry...

In view of the product life cycle, consider the progression that the EV (electric vehicle) industry is undergoing by stage. Discuss the 4 P's for each stage within the EV product journey. Be specific in describing market conditions for each stage. What are the types of buyers will the EV manufacturer encounter for each stage. How does the PLC model align with the Boston Consulting Group model in reference to the EV market? Where is the market currently for EVs?

In: Mechanical Engineering

NASA is sending a remote-sensing spacecraft to Mars. Given: Earth parking orbit altitude= 1000 km Mars...

NASA is sending a remote-sensing spacecraft to Mars.

Given:

Earth parking orbit altitude= 1000 km

Mars Parking orbit altitude=  500 km

μEarth =  3.99x105 km3/s2

μMars =  4.280x104 km3/s2

μSun =  1.33x1011 km3/s2

Earth's orbital radius =   1.50 x108 km (assume Earth has a circular orbit for this problem)

Mars' orbital radius =  2.28  x108 km (assume Mars has a circular orbit for this problem)

Find the semi major axis of the transfer orbit, v∞Earth , v∞Mars, ΔVboost,ΔVretro ,ΔVmission (enter your answer as a number which will be assumed to be in km)

In: Mechanical Engineering

All else being equal, for rolling element bearings, which is more damaging? They are equivalent. outer...

All else being equal, for rolling element bearings, which is more damaging?

They are equivalent.

outer ring rotation.

Stop worrying--they're both fine!

inner ring rotation.

In: Mechanical Engineering

A jet of water 50 mm in diameter with a velocity of 20 m/s strikes a...

A jet of water 50 mm in diameter with a velocity of 20 m/s strikes a flat plate inclined at an angle of 30° to the axis of the jet. Determine

(i) the normal force exerted on the plate when the plate is stationary

(ii) the normal force exerted on the plate when the plate is moving at 5 m/s in the direction of the jet

(iii) the work-done on the plate and the efficiency for case (ii).

In: Mechanical Engineering

The following data is provided for the spectral distribution of the radiation emitted by a diffuse...

The following data is provided for the spectral distribution of the radiation emitted by a diffuse surface.

  • Elambda (W/m2 micrometer) = 0 for lambda between 0 and 5
  • Elambda (W/m2 micrometer) = 100 for lambda between 5 and 10
  • Elambda (W/m2 micrometer) = 200 for lambda between 10 and 15
  • Elambda (W/m2 micrometer) = 100 for lambda between 15 and 20
  • Elambda (W/m2 micrometer) = 0 for lambda above 20

Provide the following:

  1. A plot of Elambda versus lambda, based on the given data
  2. Assumptions
  3. Total emissive power, E
  4. Total intensity of the radiation emitted, Ie
  5. Explain the reason why there are (or there are no) differences between the intensity emitted at 0 degrees versus at 30 degrees to the surface normal direction. Use a sketch and only one sentence.

In: Mechanical Engineering

After the experiment of Aluminum, Copper and Nylon specimens, data shows that the tangent modulus is...

After the experiment of Aluminum, Copper and Nylon specimens, data shows that the tangent modulus is lower than the Young's modulus.
What does that physically mean?
Are the specimens showing signs of softening or hardening?

In: Mechanical Engineering

given and sketch in steps the root locuse of transfer function by matlab and hand calculation...

given and sketch in steps the root locuse of transfer function by matlab and hand calculation
G(s)=(s+3)/s(s+2)

given solution please

In: Mechanical Engineering

a rocket is moving along a curve with its equation given by s=2t^3-24t+s(s in meter and...

a rocket is moving along a curve with its equation given by s=2t^3-24t+s(s in meter and t in second).

find the time required for the rocket to reach a velocity of 126 m/s from its initial condition at t=0

the acceleration of the rocket when v=0 m/s

the net displacement during the interval from t=1 s to t=4 s

draw the graphs for displacement, velocity and acceleration and explain them.

In: Mechanical Engineering

The velocity of steam at inlet to a simple impulse turbine is 1200 m/s and the...

The velocity of steam at inlet to a simple impulse turbine is 1200 m/s and the nozzle angle is 21°. The blade speed is 500 m/s and the blades are symmetrical. Evaluate:

  1. The blade angles if the steam is to enter the blades without shock. If the friction effects on the blade are negligible, specify the tangential force on the blades and the diagram power for a mass flow of 0.85 kg/s. What are the axial thrust and the diagram efficiency?
  2. If the relative velocity at exit is reduced by friction to 77 % of that at inlet, what are then the diagram power and the axial thrust? Evaluate also the diagram efficiency in this case.

In: Mechanical Engineering