Volume 23 Issue 8
Aug.  2008
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Article Navigation >  Journal of Aerospace Power  > 2008  >  23(8): 1519-1522
DING Jian-guo, ZOU Xue-qi, Wu Zhi-qing, YANG Jing-jing, HU Jun. Design and experiment demonstration of a booster of small turbofan engine[J]. Journal of Aerospace Power, 2008, 23(8): 1519-1522.
Citation: DING Jian-guo, ZOU Xue-qi, Wu Zhi-qing, YANG Jing-jing, HU Jun. Design and experiment demonstration of a booster of small turbofan engine[J]. Journal of Aerospace Power, 2008, 23(8): 1519-1522.
shu

Design and experiment demonstration of a booster of small turbofan engine

  • 1.

    College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

  • 2.

    China Aviation Power Plant Research Institute, Zhuzhou 412002, China

  • 3.

    School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 2007-08-08
  • Rev Recd Date: 2007-11-21
  • Publish Date: 2008-08-28
    Abstract
  • By means of test-proven one dimension project design procedure library and arbitrary airfoils blade design procedure of turbo machine matching the axial symmetry streamline curvature approach design code,a booster of small turbofan engine was designed and tested successfully by combining three dimension computational fluid dynamics,one dimension and two dimension aero-dynamics designs.The experiment results indicate that,the booster has high efficiency over a wider range and better stall margin,and the design results correspond with experimental results.

     

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