Volume 19 Issue 5
Oct.  2004
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TANG Hai-long, ZHU Zhi-li, LUO An-yang, ZENG Yuan-jiang. A Preliminary Analysis of Developing Series of Engines Based on an Existing Core Engine[J]. Journal of Aerospace Power, 2004, 19(5): 636-639.
Citation: TANG Hai-long, ZHU Zhi-li, LUO An-yang, ZENG Yuan-jiang. A Preliminary Analysis of Developing Series of Engines Based on an Existing Core Engine[J]. Journal of Aerospace Power, 2004, 19(5): 636-639.

A Preliminary Analysis of Developing Series of Engines Based on an Existing Core Engine

  • Received Date: 2003-09-15
  • Rev Recd Date: 2003-12-24
  • Publish Date: 2004-10-28
  • A series of engines can be derived based on an existing core engine.Components matching constraints will restrict design cycle parameter selection.A performance simulation model was established for quantitative analysis.As an example,the development of a high bypass ratio turbofan engine was used to demonstrate how the constraints restrict design cycle parameters.Preliminary analysis shows the relationship between cycle parameters and engine performance.

     

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