I have to derive an equation that determines the stagnation temperature at the turbine inlet for a turbofan engine, from some data that was measured during an experiment.
The data I have:
engine RPM
Exhaust stagnation temperature
fuel consumption
thrust
To=16C
Po=101kPa
I have...
hi,
thanks for your help. I still cannot manage to get the solution. Is there anyway you can show some working I'd appreciate it?
What I did:
Let xp = [ (cte^t+ d)w ]
therefore xp (differentiated) = cwe^t + cwte^t + 0
Then Ax(t) + g(t)
is cwte^t + [ b + 1 , -2a + 3b ]^T + [ e^t ...
Hi,
I'm having a bit of trouble with a problem here.
The question is: Use the Method of undetermined coefficients to Find the general solution to th system:
dx/dt = y + e^t
dy/dt = -2x + 3y + 1
I've got the homogenous solution fine, however I'm having a bit of difficulty with the...