SkippyBing

June 14th, 2009, 14:20

I'm fiddling with the engine tables to simulate a turbojet more accurately.

In AAM it equates Ram Drag to (V/g)*Intake Area*Table 1507*Delta t/sqrt (Theta t).

Could someone confirm that a) the units are imperial and b) what Delta t and Theta t are?!

I'm guessing it's something to do with temperature but not sure what.

In AAM it equates Ram Drag to (V/g)*Intake Area*Table 1507*Delta t/sqrt (Theta t).

Could someone confirm that a) the units are imperial and b) what Delta t and Theta t are?!

I'm guessing it's something to do with temperature but not sure what.