What is the efficiency of the engines?

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Homework Help Overview

The problem involves calculating the efficiency of aircraft engines based on power output and input during ascent. The context includes parameters such as the aircraft's weight, cruising altitude, time to reach altitude, and power delivered by the engines.

Discussion Character

  • Exploratory, Assumption checking, Mathematical reasoning

Approaches and Questions Raised

  • Participants discuss various methods to calculate acceleration and work done, with attempts to clarify the definitions of terms like initial velocity and potential energy.

Discussion Status

Some participants are exploring different equations and approaches to find the necessary parameters for calculating efficiency. There is an ongoing clarification of terms and concepts, but no consensus has been reached on the correct method or final answer.

Contextual Notes

Participants are working with specific values and units, and there seems to be some confusion regarding the application of physics equations related to motion and energy. The original poster expresses uncertainty about reaching the expected answer.

Lyphta
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Homework Statement


A 3250 km aircraft takes 12.5 minutes to achieve its cruising altitude of 10 km and cruising speed of 850 km/h. If the plane's engines deliver, on the average, 1500 hp of power during this time, what is the efficiency of the engines?


Homework Equations


Efficiency = Power output / Power input x 100
P = W/t --> P= mgh/t, P=Fdcos(theta)/t



The Attempt at a Solution


m = 3250 kg
t = 12.5 min --> 750 sec
h = 10 km --> 10000 m
Pin = 1500 hp --> 1119000 Watts
v = 850 km/h --> 236.11 m/s

vf = at +vi (attempt to find the velocity components but don't add up right)
236.11 = a (750) + 0
a = .315 m/s^2

average v = vf/2
= 236.11/2
average v = 118 m/s

Poutx = F(average v) = ma(average v)
= 3250(.315)(118)
= 120802.5 W

Piny = Fd/t = mgh/t
= 3250(9.81)(10000)/750
= 425100 W

The real answer is 4.091 x 10^8 J ; e = 48.7% but I don't know how to get that answer...
 
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Acceleration can be found by v^2 = u^2 + 2as. This acceleration is in addition to the acceleration due to gravity. So the actual acceleration of the aircraft is a+g. Now find the work done.
 
by u, do you mean initial velocity? or potential energy?
 
It is initial velocity, which is zero in this case.
 

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