Eiman
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Paper Publications
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[1]Eiman B. Saheby,.Aerodynamic design and evaluation of an open-nose supersonic drone

[2].Flow structure of the ridge integrated submerged inlet,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

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Personal information

Associate Professor

Main positions:Associate Professor

Gender:Male

Alma Mater:NUAA

Education Level:南京航空航天

Degree:Doctoral Degree in Engineering

School/Department:航空学院

Discipline:Aerospace Propulsion Theory and Engineering

Contact Information:eiman@nuaa.edu.cn

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