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Qiao Wenyou, Yu Anyuan. Overview on integrated design of inward-turning inlet with aircraft forebody[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(3): 43-59. DOI: 10.11729/syltlx20190028
Citation: Qiao Wenyou, Yu Anyuan. Overview on integrated design of inward-turning inlet with aircraft forebody[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(3): 43-59. DOI: 10.11729/syltlx20190028
shu

Overview on integrated design of inward-turning inlet with aircraft forebody

  • 1.

    Research Center of Combustion Aerodynamics, Southwest University of Science and Technology, Mianyang Sichuan 621010, China

  • 2.

    Airbreathing Hypersonic Technology Research Center of China Aerodynamics Research and Development Center, Mianyang Sichuan 621000, China

  • 3.

    Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing 210016, China

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  • Received Date: January 23, 2019
  • Revised Date: April 14, 2019
    Graphical Abstract
    • Abstract
  • The integrated design of aircraft forebody/hypersonic inward-turning inlet has become a hot spot in the research of airbreathing hypersonic propulsion system. This paper mainly analyzes the design method of hypersonic inward-turning inlet and its integration with aircraft forebody from the perspective of aerodynamic design. For the design method of the inward-turning inlet, it mainly includes direct streamline-tracing method, the osculating method with uniform incoming flow and the inverse design method based on the forebody non-uniform flow-field. The integrated design method based on the inward-turning inlet mainly includes two types:the independent intake mode facing the incoming flow and the pre-compression intake mode with the forebody. Combined with the design method of the inward-turning inlet, the design methods of these two types are analyzed in details. According to the analysis, the design method of the inward-turning inlet based on the uniform forebody flow-field has been further developed, but it is necessary to develop the design method under non-uniform incoming flow to enhance the flexibility of the integrated design. With the in-depth development of the inward-turning inlet design method, the integrated design method is bound to be further developed.
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    • References (101)
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