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Eiman
( 副教授 )
赞
的个人主页 http://faculty.nuaa.edu.cn/EIMAN/en/index.htm
副教授
性别:
男
毕业院校:
NUAA
学历:
南京航空航天
学位:
工学博士学位
所在单位:
航空学院
主要任职:
Associate Professor
联系方式:
eiman@nuaa.edu.cn
电子邮箱:
1994b04725f759f8ab13c8d9fe1d930b2d90e9d8f81f5d68071711e760961660484cce25b21e4133d6376ccfa05a908bf5b10470e88a9baf2d18a4f29c1270773878aaba585000e6b581b545de6c58cd80808a3d2e071df6fecc4ad4b7e598c5ecfc8424f809fb5fef850bba41913d8e7aa9537755d5ccac0df1d558ec9a6667
论文成果
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论文成果
[1] Eiman B. Saheby,.Aerodynamic design and evaluation of an open-nose supersonic drone
[2] .Saheby, E. B., Shen, X., Huang, G., & Hays, A. P. (2021). Flow structure of the ridge integrated ...,2021,119
[3] .Highly Integrated Inlet Design Based on the Ridge Concept,2016
[4] .The inlet flow structure of a conceptual open-nose supersonic drone,2021
[5] .Design of hypersonic forebody with submerged bump,2018
[6] .A novel aerodynamic surface for redirecting the boundary layer,2015
[7] .A novel compression surface for integration design of high speed aircraft forebody and inlet,2015
[8] .Design of Wave Derived Inlet for High Curvature Fuselage,2016
[9] .Effects of Ridge Configuration on the Performance of Integrated inlets,2016
[10] .Design of hypersonic forebody by the combination of bump and waverider surfaces,2017
[11] .Design of top mounted supersonic inlets for a cylindrical fuselage,2018
[12] .Propulsive Efficiency of Ridge/Inlet Configuration,2018
[13] .Design and numerical analysis of Mach 3.0 inlet,2017
[14] .Design of Supersonic Inlet Based on the Shock Pattern,2016
[15] .Effect of thick boundary layer ingestion on the performance of hypersonic inlet,2017
共15条 1/1
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