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Bypass ratio is one of the most important numbers used to describe a turbofan jet engine. It compares how much air flows around the engine core to how much air flows through the core where fuel is burned. Modern airliners use high-bypass turbofans because they can produce the needed thrust while using less fuel and making less noise.

This is a major reason today’s commercial jets are quieter than many older jet aircraft.

Key Facts

  • Bypass ratio = mass flow rate of bypass air ÷ mass flow rate of core air
  • BPR = m_bypass ÷ m_core
  • Total air mass flow rate = m_bypass + m_core
  • Thrust increases when the engine changes the momentum of air: F = Δp/Δt
  • For the same thrust, moving a large mass of air slowly is usually quieter than moving a small mass of air very fast.
  • High-bypass turbofans are common on airliners, while low-bypass engines are more common in older jets and some high-speed military aircraft.

Vocabulary

Bypass ratio
The ratio of the mass of air that flows around the engine core to the mass of air that flows through the engine core.
Turbofan
A jet engine that uses a large fan to send some air through the core and some air around the core.
Core flow
The air that passes through the compressor, combustion chamber, turbine, and exhaust nozzle of a jet engine.
Bypass flow
The air pushed by the fan that travels around the engine core and usually provides much of the thrust in a high-bypass turbofan.
Mass flow rate
The amount of mass passing a point each second, often measured in kilograms per second.

Common Mistakes to Avoid

  • Treating bypass ratio as a percentage is wrong because it is a ratio of two mass flow rates, not a fraction of the total flow unless it is converted carefully.
  • Thinking all thrust comes from burning fuel in the core is wrong because high-bypass turbofans get much of their thrust from fan-driven bypass air.
  • Assuming a higher exhaust speed is always better is wrong because very fast exhaust can waste energy and create more noise, especially for subsonic airliners.
  • Ignoring the difference between bypass air and core air is wrong because they follow different paths and contribute to thrust, efficiency, and noise in different ways.

Practice Questions

  1. 1 A turbofan has 320 kg/s of bypass air and 40 kg/s of core air. What is its bypass ratio?
  2. 2 An engine has a bypass ratio of 9 and a core mass flow rate of 35 kg/s. What is the bypass mass flow rate and the total mass flow rate?
  3. 3 Two engines produce the same thrust. One accelerates a small amount of air to a very high speed, while the other accelerates a large amount of air to a lower speed. Explain which is likely to be quieter for an airliner and why.