Turbofan Engines: Bypass Ratio Selection Criteria

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Discussion Overview

The discussion focuses on the criteria for selecting bypass ratios in turbofan engines, exploring the relationship between bypass ratios, engine performance, and application contexts. It includes technical considerations and varying perspectives on the factors influencing bypass ratio choices.

Discussion Character

  • Technical explanation, Debate/contested

Main Points Raised

  • One participant questions the meaning of "basis" in relation to bypass ratio selection.
  • Another participant suggests that bypass ratio selection is dictated by cycle requirements, indicating complexity in determining an optimal ratio.
  • A participant provides specific bypass ratio ranges for turbojet and turbofan engines, noting variations in thrust related to bypass ratios and questioning whether thrust or other parameters influence the selection.
  • It is proposed that the flight regime of the engine's intended use plays a significant role in bypass ratio selection, particularly emphasizing the efficiency of high bypass turbofans for commercial applications.

Areas of Agreement / Disagreement

Participants express differing views on the factors influencing bypass ratio selection, indicating that multiple competing perspectives remain without a clear consensus.

Contextual Notes

The discussion does not resolve the assumptions regarding the definitions of bypass ratios or the specific cycle requirements that may influence their selection.

vincentryan
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What Basis Bypass Ratio Has Chosen For Turbofan Engine
 
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Bypass ratios range from very small in some applications to very large in others. What do you mean by basis?
 
It's all dictated by the cycle requirements. There is no quick way to nail it down.
 
if you see bypass ratio varies from 0.1:1>br<1:1 for turbojet engine and 5:1>br<11:1 for turbofan engine.
Some turbofan engine has bypass ratio CFM 56 2c1 has 6, and CFM 56-5b3/4 has 5.3 and 5.5 has Ge 90 has 8.4 and ge 90-115b has 9 and various ratio. when your check this the thrust range is also varies with bypass ratio. is bypass ratio chosen by thrust or any other parameter.
 
It's chose by flight regime of the engine's intended use. For most commercial applications, high bypass turbofans are more efficient, as the design parameter is simply sustained high sub-mach cruise, with sufficient thrust for one engine-out performance at max gross take-off weight.
 

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