Questions
Air enters a constant diameter pipe at a pressure of 200 kPa. At the exit of...

Air enters a constant diameter pipe at a pressure of 200 kPa. At the exit of the pipe the pressure is 120 kPa, the Mach number is 0.75, and the stagnation temperature is 330°C. Determine the inlet Mach number and the heat transfer per unit mass of air.

In: Mechanical Engineering

The power source in a particular welding setup generates 3119 watts that can be transferred to...

The power source in a particular welding setup generates 3119 watts that can be transferred to the work surface with a heat transfer factor of 0.65. The metal to be welded is low carbon steel. The melting factor in the operation is 0.4. A continuous fillet weld is to be made with a cross-sectional areas of 20 mm2. Determine the travel speed in mm/s at which the welding operation can be accomplished. Hint: See Table 28.2 for the melting temperature of low carbon steel.

In: Mechanical Engineering

Air flows through a 0.25-m-diameter duct. At the inlet the velocity is 300 m/s, and the...

Air flows through a 0.25-m-diameter duct. At the inlet the velocity is 300 m/s, and the stagnation temperature is 90°C. If the Mach number at the exit is 0.3, determine the direction and the rate of heat transfer. For the same conditions at the inlet, determine the amount of heat that must be transferred to the system if the flow is to be sonic at the exit of the duct.

In: Mechanical Engineering

A journal and bearing are to be designed for a shaft that turns at 250 rpm....

A journal and bearing are to be designed for a shaft that turns at 250 rpm. Suppose
ISO VG100 (SAE Engine 30) is to be used as lubricant and the bearing length is to be equal to
1.2 times the diameter. If the no-load power loss is not to exceed 2.5 x 10-4 horsepower and the
diametral clearance is 0.0045 times the diameter, estimate the maximum diameter that can be
used for the journal, and the allowable temperature limit.

In: Mechanical Engineering

( Project question ) What do you understand by strain gauge, high light major principle and...

( Project question ) What do you understand by strain gauge, high light major principle and working differences between resistance transducer and piezoelectric transducer strain gauge. please make the font of writing clear and easy to read.

In: Mechanical Engineering

Please prove that in homogeneous nucleation of solidification the critical radius and activation energy are ??...

Please prove that in homogeneous nucleation of solidification the critical radius and activation energy are ?? ? = (? 2?????? ????? ) ( 1 ??? ) and ??? ? = ( 16???? 3???? 2 3????? 2 ) 1 ???2 , respectively, in which ? is the surface free energy, Tm is the melting temperature, ?T is the degree of supercooling (Tm - T), and ?Hf is the latent heat of fusion.

In: Mechanical Engineering

Thermodynamics 1. Correct Answer: 32.29 ± 4% A 1.4 m3 tank fills through inlet A while...

Thermodynamics

1. Correct Answer: 32.29 ± 4%

A 1.4 m3 tank fills through inlet A while supplying water through outlets B and C at the rates given below. Determine how long (minutes) it will take until the tank is full if initially the tank contains 277 kg of water. The flow rates are given in kg/min where "t" is in minutes.

All flows are at 20 C.

Mass flow rate of A = 3.5 + 2.1*t

Mass flow rate of B = 1.5

Mass flow rate of C = 1.2

2.

Correct Answer: -99.69 ± 1%

Air enters a compressor at 152 kPa and 290 K and exits at a temperature of 507.6 K. Determine the power (kW) for the compressor if the inlet volumetric flow rate is 0.244 m3 /s and the heat transfer through the shell of the compressor to the surroundings is 1.35 kW. Use the ideal gas tables (variable specific heats).

3.

(ans:19.6)

A well-insulated, full, water tank containing 198 kg of water initially at 44oC is being supplied with 15.6oC water at a rate of 4 kg/min. Water is exiting the tank at the same flow rate so that the mass of water in the tank remains constant. Circulation in the tank keeps the water at a uniform temperature. The specific heat of the water is given as C = 4.2 kJ/kg-K. Determine the time (minutes) at which the water temperature drops to 34.7oC.

Note: The energy of water in the tank is given as: E = mcv*C*T

The solution for an equation of the form: a*dT/dt + T +b = 0     is

T(t) = k1*exp(-t/a) + k2

For this problem, the given constraints are:

T(t=0) = Tinitial

T(t=infinity) = Tinlet

Hint: Use the given constraints to determine the constants k1 and k2

In: Mechanical Engineering

This is problem 7-6 from El-Wakil’s Powerplant Technology book -- a wet cooling tower receives 1.5x106...

This is problem 7-6 from El-Wakil’s Powerplant Technology book -- a wet cooling tower receives 1.5x106 lbm/min of condenser water at 96 degFahrenheit, and 1.25x106 lbm/min of air at 1 standard atmosphere, 62 degFahrenheit, and 50 percent relative humidity. The air leaves saturated at 82 degFahrenheit. Calculate (a) the exit water temperature, in degrees Fahrenheit, and (b) the percent condenser cooling water makeup due to evaporation.

In: Mechanical Engineering

This is problem 7-5 from El-Wakil’s Powerplant Technology book -- an included-draft cooling tower cools 90,000...

This is problem 7-5 from El-Wakil’s Powerplant Technology book -- an included-draft cooling tower cools 90,000 gallons per minute of water from 84 to 68 degFahrenheit. Air at 29.75 inHg absolute pressure, 70 degFahrenheit dry bulb and 60 degFahrenheit wet bulb, enters the tower and leaves saturated at 80 degFahrenheit. Find (a) the volume flow rate of air, in cubic feet per minute, and (b) the makeup water required, in pound mass per hour.

In: Mechanical Engineering

Compare the three types of lubrication systems for plain bearings using sketches and Bearing Parameter/ Stribeck...

Compare the three types of lubrication systems for plain bearings using sketches and Bearing Parameter/ Stribeck Curve.

In: Mechanical Engineering

What are Fixed side and Floating side bearing arrangement? Explain their applications with sketches.

What are Fixed side and Floating side bearing arrangement? Explain their applications with sketches.

In: Mechanical Engineering

An airfoil profile to be used on a wind turbine blade is tested in a wind...

An airfoil profile to be used on a wind turbine blade is tested in a wind tunnel. The prototype (full-scale) airfoil section has a chord length of 2m and moves at 50 m/s relative to the wind, the wind tunnel model has a chord length of 0.4m. The temperature for the model test is the same as for prototype operation.

(a) What criterion should be used to obtain dynamic similarity in the experiment? (Write out the criterion in an equation.) (b) What velocity should the wind tunnel be operated at to have dynamic similarity for the scale model? (assuming tests at atmospheric pressure.) (c) The wind tunnel available for this test can only be operated at 100 m/s, but it can also be pressurized. What pressure should be used in the wind tunnel to have dynamic similarity? (Assume the air behaves like an ideal gas.)

In: Mechanical Engineering

Along, square, electrical heating element standing on a corner with one side of the square heating...

Along, square, electrical heating element standing on a corner with one side of the square heating element being 25mm, thermal conductivity k = 240 W/m ? K, density ñ = 2700 kg/m3, and specific heat cp = 900 J/kg ? K is installed in a duct for which air moves in cross flow over the heater at a temperature and velocity of 30°C and 10 m/s, respectively.

(a) Neglecting radiation, estimate the steady-state surface temperature when, per unit length of the heater, electrical energy is being dissipated at a rate of 1000 W/m. ?

(b) If the heater is activated from an initial temperature of 30°C, estimate the time required for the surface temperature to come within 20°C of its steady-state value. ?

In: Mechanical Engineering

what are the differences of all these cooling load calculation methods? What are the full name...

what are the differences of all these cooling load calculation methods? What are the full name of these methods and the strength and limitation of these approaches?

a)HB method

b)CLTD method

c)RTS method

In: Mechanical Engineering

At an altitude where the air is at 35 kPa and -40°C a turbojet aircraft flies...

At an altitude where the air is at 35 kPa and -40°C a turbojet aircraft flies with a velocity of 260 m/s. Compressor has a pressure ratio of 10, and the temperature of the gases at the turbine inlet is 1100°C. Air enters the compressor at a rate of 45 kg/s.
*Part(A)* Use *hot air standard assumptions* to find
(a) the temperature and pressure of the gases at the turbine exit
(b) the velocity of the gases at the nozzle exit
(c) the propulsive efficiency of the cycle
*Part(B)* Use *cold air standard assumptions* to find
(a) the temperature and pressure of the gases at the turbine exit
(b) the velocity of the gases at the nozzle exit
(c) the propulsive efficiency of the cycle

In: Mechanical Engineering