subject
Engineering, 17.04.2020 18:17 Izayoi

An ideal turbojet ingests 192 lbm/s of air at an altitude of 22000ft it flies at a mach number of 0.88 and the compressure pressure ratio is 17 the fuel has a heating value of 17900 and the burner exit total temperature is 2350 find the developed thrust dimensionless thrust and TSFC..

ansver
Answers: 2

Another question on Engineering

question
Engineering, 03.07.2019 14:10
The y form of iron is known as: a) ferrite b) cementite c) perlite d) austenite
Answers: 3
question
Engineering, 04.07.2019 18:10
Aloaded platform of total mass 500 kg is supported by a dashpot and by a set of springs of effective stiffness 72 kn/m. it is observed that when the platform is depressed through a distance x = 12.5 cm below its equilibrium position and then released without any initial velocity; it reaches its equilibrium position in the shortest possible time without overshoot. find the position and velocity of the loaded platform 0.10 sec. after its release. if a further load of 400 kg is added to the platform, find, i) the frequency of damped vibrations, and i) the amplitude of vibration after 2 complete oscillations, given that the initial amplitude is 15 cm.
Answers: 1
question
Engineering, 04.07.2019 18:10
Aflywheel accelerates for 5 seconds at 2 rad/s2 from a speed of 20 rpm. determine the total number of revolutions of the flywheel during the period of its acceleration. a.5.65 b.8.43 c. 723 d.6.86
Answers: 2
question
Engineering, 04.07.2019 18:10
Burgers vector is generally parallel to the dislocation line. a)-true b)-false
Answers: 2
You know the right answer?
An ideal turbojet ingests 192 lbm/s of air at an altitude of 22000ft it flies at a mach number of 0....
Questions
question
Physics, 02.03.2021 01:20
question
Mathematics, 02.03.2021 01:20
question
English, 02.03.2021 01:20
question
Mathematics, 02.03.2021 01:20
question
Health, 02.03.2021 01:20
question
Mathematics, 02.03.2021 01:20
Questions on the website: 13722362