7-9. Products of combustion enter the afterburner (station 6) at a rate of 230 lbm/sec with the following propertie...
7-9. Products of combustion enter the afterburner (station 6) at a rate of 230 lbm/sec with the following properties: T%-1830°R, P638 psia, M6-0.4, y 1.33, cp 0.276 Btu/(lbm.°R), and R 53.34 ft Ibf/(lbm "R). Assume a calorically perfect gas and B 0.95. a. Determine the flow area at station 6 in square feet. b. With the afterburner off, determine the area (ft) of the exhaust nozzle's choked throat (station 8) for P8//%-0.97 c. With the afterburner on, determine the afterburner fuel flow rate (lbm/sec) and the area (ft) of the exhaust nozzle's choked throat (station 8) for Ps Pr6-0.94 and Ts 3660 R. Assume that the gas leaving the operating afterburner (part c) is a calorically perfect gas with y-1.3, cp- 0.297 Btu/(lbm R), and the same gas constant. Also assume the properties at station 6 do not change and hR 18,400 Btu/lbm 0.94 and Is
7-9. Products of combustion enter the afterburner (station 6) at a rate of 230 lbm/sec with the following properties: T%-1830°R, P638 psia, M6-0.4, y 1.33, cp 0.276 Btu/(lbm.°R), and R 53.34 ft Ibf/(lbm "R). Assume a calorically perfect gas and B 0.95. a. Determine the flow area at station 6 in square feet. b. With the afterburner off, determine the area (ft) of the exhaust nozzle's choked throat (station 8) for P8//%-0.97 c. With the afterburner on, determine the afterburner fuel flow rate (lbm/sec) and the area (ft) of the exhaust nozzle's choked throat (station 8) for Ps Pr6-0.94 and Ts 3660 R. Assume that the gas leaving the operating afterburner (part c) is a calorically perfect gas with y-1.3, cp- 0.297 Btu/(lbm R), and the same gas constant. Also assume the properties at station 6 do not change and hR 18,400 Btu/lbm 0.94 and Is