thrust in propeller engines


by Emzielou83
Tags: engines, propeller, thrust
Emzielou83
Emzielou83 is offline
#1
Dec8-10, 08:44 AM
P: 23
Can anyone help me?

I'm doing a question on aircraft propulsion technology and i'm stuck.

The question is:

'If the mass of air through a propeller is 1000 Kg/s, the aircraft's velocity is 100 m/s and the slipstream velocity is 120 m/s, calculate the thrust?

Attempt at answer:

Surely if F = ma then the equation should be F = 1000 * 100 = 10000 Kg/s

But I don't think this is the right answer as I have not taken the slipstream velocity in to consideration.

The only other equation I can find is

F = (m dot * V)e - (m dot * V)0 + (pe - p0) * Ae

But I don't have pe or p0 or Ae neither do I understand what they are.


Can someone please steer me in the right direction?

Thanks
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avinod4all
avinod4all is offline
#2
Dec8-10, 01:01 PM
P: 8
Hi, with the given conditions, thrust can be calculated by using the formula:
Thrust = Mass airflow X (slipstream velocity-aircraft velocity).
Below website has good information may be it helps you.

http://www.flightlearnings.com/basic...-part-two/384/
Emzielou83
Emzielou83 is offline
#3
Dec8-10, 01:36 PM
P: 23
Thanks very much.

It seems so simple now, just couldn't see it.

Thanks again


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