Turbofan Engines: Bypass Ratio Selection Criteria

Click For Summary
SUMMARY

The discussion focuses on the selection criteria for bypass ratios in turbofan engines, emphasizing that these ratios range from 0.1:1 for turbojet engines to between 5:1 and 11:1 for turbofan engines. Specific examples include the CFM 56-2C1 with a bypass ratio of 6, the CFM 56-5B3/4 with ratios of 5.3 and 5.5, and the GE90 series with ratios of 8.4 and 9. The choice of bypass ratio is dictated by the engine's intended flight regime and performance requirements, particularly for commercial applications where high bypass turbofans offer greater efficiency and thrust capabilities.

PREREQUISITES
  • Understanding of turbofan engine design principles
  • Familiarity with thrust-to-weight ratios in aviation
  • Knowledge of flight regimes and their impact on engine performance
  • Basic concepts of engine cycle requirements
NEXT STEPS
  • Research the design parameters of high bypass turbofan engines
  • Explore the performance characteristics of the GE90 engine series
  • Learn about the impact of bypass ratio on fuel efficiency in commercial aviation
  • Investigate the relationship between thrust requirements and bypass ratio selection
USEFUL FOR

Aerospace engineers, aviation students, and professionals involved in aircraft engine design and performance optimization will benefit from this discussion.

vincentryan
Messages
28
Reaction score
0
What Basis Bypass Ratio Has Chosen For Turbofan Engine
 
Physics news on Phys.org
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.
 

Similar threads

Replies
5
Views
3K
  • · Replies 16 ·
Replies
16
Views
4K
Replies
0
Views
262
  • · Replies 4 ·
Replies
4
Views
5K
  • · Replies 5 ·
Replies
5
Views
3K
  • · Replies 2 ·
Replies
2
Views
6K
  • · Replies 5 ·
Replies
5
Views
7K
  • · Replies 2 ·
Replies
2
Views
1K
  • · Replies 1 ·
Replies
1
Views
7K
Replies
2
Views
3K