Aircraft Propulsion, Other Engineering




An aircraft is flying at a speed of 500 ft/s an altitude of 20,000 ft, where the atmospheric
temperature and pressure are 447.3°R and 972.5 lbf/ft2, respectively. If the inlet / diffuser
adiabatic efficiency is ?d = 0.92, compute the stagnation temperature and pressure at the
compressor face.



Rair = 1716 ft2/s2 –R cp,cold = 0.24 Btu/lbm-R cp,hot = 0.276 Btu/lbm-R cpAB = 0.29 Btu/lbm-R
?cold = 1.4 ?hot = 1.33 ?AB = 1.30
Posted Date: 4/8/2013 1:51:43 PM | Location : United States







Related Discussions:- Aircraft Propulsion, Assignment Help, Ask Question on Aircraft Propulsion, Get Answer, Expert's Help, Aircraft Propulsion Discussions

Write discussion on Aircraft Propulsion
Your posts are moderated
Related Questions
The firm is considering an investment opportunity. The investment falls in the same class of risk as the firm, the project is financed with equity and debt. Explain all the steps i

need help correcting an error on running the developed app it doesnt show the fetched output from internet ?

Duct With Flow Control-Aircraft maintenance: BERNOULLI'S THEOREM This theorem can be related to the relationship between pressure and velocity existing in the air flowing

Direct probe,isolation probe,high impedence probe,active probe,current probe

characteristic equation The characteristic equation (C.E.) corresponding to the linear state space equations comprising the state equation? x = Ax + Bu and output equatio

Continuous Casting : In essential, the process consists of pouring molten metal into a short vertical metal die or mould (at a controlled rate), which is open at both ends, coolin

what do you know about area and volume by contour?explain

what is covered un this field?

Bay cooling in Aircraft: There are two methods of bay cooling, they are: • Ram air cooling • Fan air cooling RAM AIR COOLING For ram air cooling, the aircraft has to

Expertsmind.com brings you unique solution in electrical engineering Class A Amplifier Operation Class A amplifiers are biased so that variations in input signal polarit