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

Qiao Wenyou; Yu Anyuan

doi:10.11729/syltlx20190028

Volume 33 Issue 3

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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

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

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

doi: 10.11729/syltlx20190028

Qiao Wenyou^{1, 3
,
,},
Yu Anyuan²

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

Received Date: 2019-01-24
Rev Recd Date: 2019-04-15
Publish Date: 2019-06-25

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.
- hypersonic,
- inward-turning inlet,
- integration,
- waverider,
- aircraft forebody

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References(101)

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