WorksheetsEnergy Conversion Quiz 2 Review
Total questions: 13
Worksheet time: 25mins
On a log P-h diagram, what does the horizontal axis represent?
Entropy
Enthalpy
Internal Energy
Empathy
On this log p - h diagram, what does the green highlighted curve represent?
Constant Pressure
Constant Enthalpy
Constant Entropy
Constant Temperature
Select all statements that are true about CLOSED feedwater heaters:
They are reversible
No heat or work input
All flows must be at the same pressure
Enthalpy flowrate in = enthalpy flowrate out
equal number of inlets and outlets
Select all statements that are true about OPEN feedwater heaters:
They are reversible
No heat or work input
All flows must be at the same pressure
Enthalpy flowrate in = enthalpy flowrate out
equal number of inlets and outlets
An open feedwater heater operates at 0.6 MPa, where 2 streams enter and one leaves. One (1) of the entering streams is a 2-phase liquid-vapour mix. The exiting stream from the heater (3) is a SATURATED LIQUID.
What must be the state of the other entering stream (2)?
Compressed liquid
Saturated liquid
2-phase mix
Saturated vapour
An adiabatic compressor takes in air at p1, compresses it with a work input, and outputs the air at p2.
For the lowest possible work requirement, what is true about the entropies before and after compression (s1 and s2)?
s2 = s1
s2 > s1
s2 < s1
A non-adiabatic compression device (exchanges both work and heat) takes in air at p1 and outputs it at p2.
For the lowest possible work requirement, what is true about the entropies before and after compression (s1 and s2)?
s2 = s1
s2 > s1
s2 < s1
What is true about the utilization factor εu in cogeneration plants?
εu=qBwnet+qP
Can be greater than 1
Considers all heat and work exchanged
Can be greater than the Carnot efficiency
Which of the following are advantages of a Bypass Turbofan engine compared to a Standard Turbojet engine?
Increased mass flow rate
Increased exit velocities
Less work extracted from turbine
Higher propulsive efficiency
The exhaust of this Laval nozzle has Ma = 3. What is the velocity at the throat?
v = 0
v < a
v = a
v > a
A Laval Nozzle has sonic flow in the throat but a subsonic exit velocity. Select all statements that are possible.
The flow decelerates isentropically past the throat
The flow undergoes a shock outside the nozzle
The flow undergoes a shock within the nozzle
This flow arrangement is not possible
Which of these related courses would you like to take in the future? (Select any that you've already taken too)
MECH442: HVAC
MECH442: Advanced Thermodynamics
MECH450C (Fall term): Energy Conversion and Storage
MECH492: Transport Phenomena
Ew, no more thermo-related courses for me!
Thank you!!!
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