Author

Eiman B. Saheby

Observed names: E. B. Saheby, Eiman B Saheby, Eiman Bondar Saheby

Institution: Nanjing University of Aeronautics and Astronautics

Observed institution: Nanjing University of Aeronautics and Astronautics

ORCID: 0000-0001-7153-3427

Observed ORCID: 0000-0001-7153-3427

OpenAlex ID: A5042619374

Design and performance study of a parametric diverterless supersonic inlet

2019 · Eiman B Saheby, Xing Shen, et al. · Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering · 18

Flow structure of the ridge integrated submerged inlet

2021 · Eiman B. Saheby, Xing Shen, et al. · Aerospace Science and Technology · 13

Highly Integrated Inlet Design Based on the Ridge Concept

2016 · Eiman B. Saheby, Huang Gouping, et al. · Journal of Propulsion and Power · 12

Design of top mounted supersonic inlets for a cylindrical fuselage

2018 · Eiman B Saheby, Huang Gouping, et al. · Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering · 7

Design of hypersonic forebody with submerged bump

2018 · Eiman B Saheby, Huang Guoping, et al. · Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering · 6

Impact of internal lattice structures on the weight and natural frequencies of a low pressure turbine blade

2024 · Muhammad U Safdar, Xing Shen, et al. · Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering · 4

Propulsive Efficiency of Ridge/Inlet Configuration

2018 · Guoping Huang, Eiman B. Saheby, et al. · International Journal of Aerospace Engineering · 4

Aerodynamic design and evaluation of an open-nose supersonic drone

2022 · Eiman B. Saheby, Anthony P. Hays, et al. · Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering · 3

Effects of Ridge Configuration on the Performance of Integrated inlets

2016 · Gouping Huang, Eiman B. Saheby, et al. · AIAA/SAE/ASEE Joint Propulsion Conference (JPC) · 3

The impact of BCC lattice structure on low-pressure turbine blade structural dynamics

2025 · Muhammad Usman Safdar, Xing Shen, et al. · Proceedings of the Institution of Mechanical Engineers Part C Journal of Mechanical Engineering Science · 2

Location-Based Integration of Internal Lattice Structures in a Turbine Blade for Mass Reduction and Dynamic Characteristic Comparison

2024 · M. U. Safdar, X. Shen, et al. · International Journal of Aeronautical and Space Sciences · 2

Design of hypersonic forebody by the combination of bump and waverider surfaces

2017 · Eiman B. Saheby, Guoping Huang, et al. · AIAA International Space Planes and Hypersonic Systems and Technologies Conference · 2

Design of Wave Derived Inlet for High Curvature Fuselage

2016 · Eiman B. Saheby, Gouping Huang, et al. · AIAA/SAE/ASEE Joint Propulsion Conference (JPC) · 2

A novel compression surface for integration design of high speed aircraft forebody and inlet

2015 · Eiman B. Saheby, Guoping Huang, et al. · AIAA International Space Planes and Hypersonic Systems and Technologies Conference · 2

Aero-elastic response of structurally modified turbine blades

2025 · Muhammad Usman Safdar, Xing Shen, et al. · Aircraft Engineering and Aerospace Technology · 1

Aerodynamic efficiency analysis of the ridge integrated submerged inlet

2024 · Eiman B Saheby, Xing Shen, et al. · Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering · 1

The inlet flow structure of a conceptual open-nose supersonic drone

2021 · Eiman B Saheby, Xing Shen, et al. · Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering · 1

A novel aerodynamic surface for redirecting the boundary layer

2015 · Eiman B. Saheby, Guoping Huang, et al. · AIAA Applied Aerodynamics Conference · 1

Aeroelastic stability evaluation of structurally enhanced low-pressure turbine blade

2025 · Muhammad Usman Safdar, Xing Shen, et al. · Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering

Vortex behavior over a tailless forward-swept wing with chine forebody configuration

2025 · Eiman B. Saheby, Li Jialu, et al. · Aerospace Science and Technology

Works count: 20

Citation count: 84

H-index: 5

I10-index: 3