Jet engines at High altitudes
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Joined: Nov 2007
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From: Turning outbound
Jet engines at High altitudes
Hey Chaps
I'm doing some private studies on Aerodynamics but there's something i'm clearly battling to understand,can anybody explain me why a jet engine is very fuel efficient at High altitudes?
I'm doing some private studies on Aerodynamics but there's something i'm clearly battling to understand,can anybody explain me why a jet engine is very fuel efficient at High altitudes?

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From: Switzerland
Joined: Oct 2010
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From: Nairobi
engine performance
At high altitudes,the air is thinner.
1. thermal efficency greater at higher temp differentials, engine is a heat pump the hotter the efflux the more efficient the burn.
2. compressors work better at high rpms, hi altitude flight allows more rpm without exceeding thrust/airframe speed limitations
3. reduced friction/drag at altitudes allowing lower output at altitude, while retaining a set mach/airspeed. better SFC
1. thermal efficency greater at higher temp differentials, engine is a heat pump the hotter the efflux the more efficient the burn.
2. compressors work better at high rpms, hi altitude flight allows more rpm without exceeding thrust/airframe speed limitations
3. reduced friction/drag at altitudes allowing lower output at altitude, while retaining a set mach/airspeed. better SFC
Joined: Apr 2009
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From: somewhere in the sky
In other words, the thrust produced by a jet engine is given as rpm which is a function of air density. Density is dependent on pressure and temperature. With the temperature drop at higher altitudes, the thrust increases and the Specific Fuel Consumption of a jet engine is decreased, the performance is improved and the endurance is increased.
Good luck.
Good luck.
Joined: Apr 2009
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From: down south
There is , of course, also the question of propulsive efficiency, as shown by the Froude formula:
TAS x 2 divided by (TAS plus exhaust velocity).
Propulsive efficiency is higher when, for a given exhaust velocity, the true airspeed is higher ie at altitude.
TAS x 2 divided by (TAS plus exhaust velocity).
Propulsive efficiency is higher when, for a given exhaust velocity, the true airspeed is higher ie at altitude.




