Jet-Wing Interaction Flow Field Study for Missiles in Supersonic Free Streams
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- 所属单位：航空学院
- 发表刊物：Proc. Int. Conf. Mech. Aerosp. Eng., ICMAE
- 摘要：The flow field structure of the lateral jet flow ejected into supersonic free stream over missile bodies with and without X-shape front wings is numerically studied. Results of seven jet exit locations for two geometries are analyzed and compared. The interaction between jet flow and front wings contributes several favorable factors for maneuvering control namely the wraparound effect obstruction, another high pressure region behind the wake and extra advantaged interaction force on wings. © 2018 IEEE.
- 是否译文：否
- 发表时间：2018-09-18
- 合写作者：Li, Longfei,Wang, Yuhan,Zhao, Faming
- 通讯作者：Li, Longfei,王江峰
- 发表时间：2018-09-18
