Comparing turboprop and turbofan

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SUMMARY

This discussion focuses on comparing turboprop and turbofan engines, specifically their specific power and thrust-specific fuel consumption (TSFC). Turbofans are rated in Newtons, and their power can be calculated using the formula THP = (T * MPH) / 375, where THP represents thrust horsepower. A more relevant metric for comparison is TSFC, defined as T_{SFC} = \dot{m_f} / T, which evaluates the efficiency of thrust relative to fuel consumption. The discussion references Chapter 1 of an AIAA document for further insights on overall efficiency and related metrics.

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balogun
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i am involved in a project that involves comparing turboprop to trubofan.I want to compare their specific power .but turbofans are rated in Newtons.can the power of a turbofan be calcuated by multiplying its thrust with speed of the aircraft at that thrust.
 
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Yes. There is a, although outdated method, that is called thrust horsepower. It is uses a selected reference speed of 375 MPH that the math works out 1 pound of thrust to 1 HP.

THP=\frac{T*MPH}{375}

Really, a more substantial and meaningful comparison is in thrust SFC or Thrust Specific Fuel Consumption.

T_{SFC}=\frac{\dot{m_f}}{T}
 
Chapter 1 of http://www.aiaa.org/content.cfm?pageid=360&id=1343" defines a quantity called "overall efficiency," which is the thrust power divided by the rate of heat addition from the fuel. Other quantities of interest include specific thrust and fuel air ratio (from which TSFC can be found).
 
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