Question

The rate of heat addition to an air-standard Brayton cycle is 3.4 times 109 Btu/h. The...

The rate of heat addition to an air-standard Brayton cycle is 3.4 times 109 Btu/h. The pressure ratio for the cycle is 15 and the minimum and maximum temperatures are 520°R and 3000°R, respectively. Determine (a) the thermal efficiency of the cycle. (b) the mass flow rate of air, in lb/h. (c) the net power developed by the cycle, in Btu/h.

Homework Answers

Answer #1

The cycle will have two isobaric and two reversible processes

T1=520R. T3= 3000R

rp= compression ratio = 15, Y= ratio of specific heats for air = 1.4

Thermal efficiency = 1- 1/(rp)(Y-1)/Y    =1 -1/(15)0.4/1.4= 0.5387 or 53.87%

T2/T1= (rP) (Y-1)/Y= 15 (0.4/1.4) =2.17, T2= 520*2.17= 1128.4 R

T3/T4= 1.67, T3= 3200/1.67= 1916 R

Cp =0.244 Btu/lb.R

WC= 0.244*(1128.4-520)= 148 Btu/lb

WT= 0.244*(3000-1916)=264.49 Btu/lb

Work ratio = (WT-WC)/WT= (264.49-148)/264.49=0.44

Power output= 3.4*109*0.44 btu/hr=163.06 Btu/hr

m*Cp*(1916-1128.4)= 3.4*109

Cp =0.244

m = 5.74 lb/hr

Know the answer?
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for?
Ask your own homework help question
Similar Questions
You’ve developed a cold air standard Brayton cycle with input from combustion of 5.0×10^6 Btu/h with...
You’ve developed a cold air standard Brayton cycle with input from combustion of 5.0×10^6 Btu/h with a mass flow rate of 6 lb(mass)/s. Air enters the turbine at 2800°R and exit at 520°R the cycle has a compression pressure ratio of 12. If the specific heat is evaluated at 500°R and the turbine and compressor both have isentropic and chopping efficiencies of 95%. what is the net power developed by the cycle in hp.
Air enters the compressor of an air-standard Brayton cycle with a volumetric flow rate of 60...
Air enters the compressor of an air-standard Brayton cycle with a volumetric flow rate of 60 m3/s at 0.8 bar, 280 K. The compressor pressure ratio is 17.5, and the maximum cycle temperature is 1950 K. For the compressor, the isentropic efficiency is 92% and for the turbine the isentropic efficiency is 95%. Determine: (a) the net power developed, in kW. (b) the rate of heat addition in the combustor, in kW. (c) the percent thermal efficiency of the cycle.
An air-standard Brayton cycle has a compressor pressure ratio of 10. Air enters the compressor at...
An air-standard Brayton cycle has a compressor pressure ratio of 10. Air enters the compressor at p1 = 14.7 lbf/in.2, T1 = 70°F, with a mass flow rate of 90,000 lb/h. The turbine inlet temperature is 1800°R. Calculate the thermal efficiency and the net power developed, in horsepower, if (a) the turbine and compressor isentropic efficiencies are each 100%. % hp (b) the turbine and compressor isentropic efficiencies are 88 and 84%, respectively. % hp (c) the turbine and compressor...
the ideal air standard Brayton cycle consists of the following processes: 1-2 isentropic compression through a...
the ideal air standard Brayton cycle consists of the following processes: 1-2 isentropic compression through a pressur ratio rp =p2/p1 2-3 heat addition at constant pressure untill the pressure is p3 3-4 isentropic expansion to the initial pressure 4-1 heat rejection at constnt pressure A- show that the cycle efficiency for this cycle is B-Air enters compressor of a gas turbine at 100kpa and 250c.for a pressure ratio of 5 and a maximum temp of 8500c , determine the thermal...
Air enters the compressor of a simple gas turbine at p1 = 14 lbf/in2, T1 =...
Air enters the compressor of a simple gas turbine at p1 = 14 lbf/in2, T1 = 520°R. The isentropic efficiencies of the compressor and turbine are 83 and 87%, respectively. The compressor pressure ratio is 16 and the temperature at the turbine inlet is 2500°R. The volumetric flow rate of the air entering the compressor is 9000 ft3/min. Use an air-standard analysis. Determine all temperatures at each state. A) Determine the net power developed, in Btu/h. (Already did this part,...
A simple Brayton cycle using air as the working fluid has a pressure ratio of 10....
A simple Brayton cycle using air as the working fluid has a pressure ratio of 10. The minimum and maximum temperatures in the cycle are 295 and 1240 K. Assuming air standard analysis, determine (a) the air temperature at the turbine exit, (b) the net-work output (in kJ/kg), and (c) the thermal efficiency.
Incorrect answer. Your answer is incorrect. Try again. An air-standard Brayton cycle has a compressor pressure...
Incorrect answer. Your answer is incorrect. Try again. An air-standard Brayton cycle has a compressor pressure ratio of 10. Air enters the compressor at p1 = 14.7 lbf/in.2, T1 = 70°F, with a mass flow rate of 90,000 lb/h. The turbine inlet temperature is 1900°R. Calculate the thermal efficiency and the net power developed, in horsepower, if (a) the turbine and compressor isentropic efficiencies are each 100%. Entry field with incorrect answer 47.56 % Entry field with incorrect answer 5468.73...
The compression ratio of an air-standard Diesel cycle is 17 and the conditions at the beginning...
The compression ratio of an air-standard Diesel cycle is 17 and the conditions at the beginning of compression are p1 = 14.0 lbf/in.2, V1 = 2 ft3, and T1 = 520°R. The maximum temperature in the cycle is 4000°R. Calculate (a) the net work for the cycle, in Btu. Btu (b) the thermal efficiency. % (c) the mean effective pressure, in lbf/in.2 lbf/in.2 (d) the cutoff ratio.
n ideal air-standard Brayton cycle operates at steady state with compressor inlet conditions of 290 K...
n ideal air-standard Brayton cycle operates at steady state with compressor inlet conditions of 290 K and 95 kPa and a fixed turbine inlet temperature of 1650 K. For a compressor pressure ratio of 10, determine: (a) the exhaust temperature of the cycle, in K. (b) the back work ratio. (c) the net work developed per unit mass flowing, in kJ/kg. (d) the heat addition per unit mass flowing, in kJ/kg. (e) the thermal efficiency for the cycle.
7.2 A Brayton cycle gas engine is analyzed using the air standard method. Given the conditions...
7.2 A Brayton cycle gas engine is analyzed using the air standard method. Given the conditions at state 1, pressure ratio (rp), and cutoff ratio (rc) determine the efficiency and other values listed below. The specific heat ratio and gas constant for air is given as k=1.4 and R=0.287 kJ/kg-K respectively. T1 (K) = 333 P1 (kPa) = 170 rp = 10.7 rc = 2.54 AV (m3/s) = 1.7 a) Determine the specific enthalpy (kJ/kg) at state 1. b) Determine...