Affiliation of Author(s):航空学院
Journal:Proc. Int. Conf. Mech. Aerosp. Eng., ICMAE
Abstract: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.
Translation or Not:no
Date of Publication:2018-09-18
Co-author:Li, Longfei,Wang, Yuhan,Zhao, Faming
Correspondence Author:Li, Longfei,WANG Jiangfeng
Professor
Supervisor of Doctorate Candidates
Gender:Male
Alma Mater:南京航空航天大学； Université Pierre et Marie Curie
Education Level:法国巴黎第六大学
Degree:Doctoral Degree in Engineering
School/Department:College of Aerospace Engineering
Discipline:Fluid Mechanics. Fluid Mechanics
Business Address:本部流体楼（C12）- 301室
Contact Information:wangjf@nuaa.edu.cn
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