プロフィール詳細

プロジェクトを作成

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Dr. M S.に依頼

United Kingdom

Expert in Computational Aerodynamics, providing consultancy in OpenFOAM Development, Testing of Aerospace & Automative

プロフィール概要

I have 15+ years of experience in Fluid dynamics & Flight Dynamics. I can develop custom codes for your company in OpenFOAM, I already have many solvers that outperform the default solvers. I can help generate outstanding grids which help to reduce convergence time and I help companies reduce turnover time in design testing and validation stage for both aeronautical and automotive related concepts.

専門分野

• ☆ Aerospace Engineering
• ☆ Aeronautics
• ☆ Fluid Mechanics
• ☆ Computational Fluid Dynamics
• ☆ Fluid Dynamics

サービス

• Research
• Consulting
• Data & AI
• Product Development

Research User Research, Feasibility Study, Fact Checking, Gap Analysis, Scientific and Technical Research, Systematic Literature Review

Consulting Scientific and Technical Consulting

Data & AI Predictive Modeling, Algorithm Design-Non ML, Algorithm Design-ML, Data Visualization

Product Development Product Validation, Concept Development, Product Launch Support

職務経験

Assistant Professor (Guest)

Coventry University

7月 2025 - 現在

Senior Lecturer

De Montfort University Leicester

6月 2022 - 現在

Researcher at NASA/AIAA High Lift Predition Workshop 5

Meshing Focus Group HLPW-5

1月 2024 - 1月 2025

Research Fellow in Computational Aerodynamics

De Montfort University Leicester

10月 2019 - 8月 2021

学歴

PhD in Computational Aerodynamics and Flight Dynamics (School of Engineering)

De Montfort University

10月 2015 - 6月 2019

MSc in Mechanical Engineering

De Montfort University Leicester - United Kingdom

6月 2014 - 8月 2015

認定資格

• OpenFOAM certification

  American Institue of Aeronautics & Astronautics

  1月 2023 - 現在

出版物

JOURNAL ARTICLE

Mohamed Sereez, Mikhail Goman, Nikolay Abramov, Caroline Lambert (2025). Numerical Simulation of Self-Sustained Roll Oscillations of an 80-Degree Delta Wing Caused by Leading-Edge Vortices . Aerospace.

Mohamed Sereez, Mikhail Goman, Nikolay Abramov, Caroline Lambert (2025). Numerical Simulation of Self-Sustained Roll Oscillations of an 80-Degree Delta Wing Caused by Leading-Edge Vortices . Aerospace.

Mohamed Sereez, Nikolay Abramov, Mikhail Goman (2024). CFD Simulations and Phenomenological Modelling of Aerodynamic Stall Hysteresis of NACA 0018 Wing . Aerospace.

Mohamed Sereez, Nikolay Abramov, Mikhail Goman (2024). CFD Simulations and Phenomenological Modelling of Aerodynamic Stall Hysteresis of NACA 0018 Wing . Aerospace.

M. Sereez, N. Abramov, M. Goman (2023). Prediction of aerodynamic characteristics of high-lift Common Research Model in ground effect . The Aeronautical Journal.

Mohamed Sereez, Nikolay Abramov, Mikhail Goman (2023). A modified dual time integration technique for aerodynamic quasi-static and dynamic stall hysteresis . Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering.

Mohamed Sereez, Mikhail Goman(2022). Evaluation of Aerodynamic Characteristics in Oscillatory Coning Motion Using CFD Methods . Proceedings of the 9th European Conference for Aerospace Sciences. Lille, France, 27 June - 1 July, 2022. Proceedings of the 9th European Conference for Aerospace Sciences. Lille, France, 27 June - 1 July, 2022

(2018). Impact of Ground Effect on Airplane Lateral Directional Stability during Take-Off and Landing . Open Journal of Fluid Dynamics.

(20). Computational Ground Effect Aerodynamics and Airplane Stability Analysis During Take-off and Landing . Proceedings of the 7th European Conference for Aeronautics and Space Sciences. Milano, Italy, 3-6 july 2017.

Prediction of Static Aerodynamic Hysteresis on a Thin Airfoil Using OpenFOAM . Journal of Aircraft.

CONFERENCE PRESENTATION

RANS Prediction of Aerodynamic Characteristics of CRM-HL Configuration Using OpenFOAM for the HLPW-5 @conference{3a90d3b9e81143d19602440bf4eab026, title = "RANS Prediction of Aerodynamic Characteristics of CRM-HL Configuration Using OpenFOAM for the HLPW-5", abstract = "This paper presents the results of numerical simulations obtained during the work of the RANS Technology Research Group (RANS-TFG) (subgroup R-004) within the framework of the High Lift Prediction Workshop 5. The computational simulations were performed using the open source CFD code Open FOAM and the required meshes were generated using ICEM CFD software and Siemens Star-CCM+ code, which are capable of generating high quality structured/unstructured grids compatible with the Open FOAM platform. Group R-004 was focused on two major studies: Test case 1, the verification case for a pre-stall angle of attack considering a wing-body configuration and Test case 2, the configuration build-up study with gradual increase of geometry complexity by adding horizontal tail, vertical tail, fairings, slats and slat tracks, flaps and finally nacelle-pylons. The agreement of RANS simulations results with experimental data as the complexity of the geometry increases is assessed along with the residuals convergence and sufficient grid independence. RANS simulation results are presented and discussed showing the presence of static aerodynamic hysteresis for Test Case 1 and Test Case 2.2, which exhibit two different flow separation patterns at the same angle of attack.", author = "Mohamed Sereez and Caroline Lambert and Mikhail Goman", note = "Publisher Copyright: {\textcopyright} 2025, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA SCITECH 2025 Forum ; Conference date: 06-01-2025 Through 10-01-2025", year = "2025", month = jan, day = "6", doi = "10.2514/6.2025-0275", language = "English", } . AIAA SCITECH 2025 Forum, Orlando, United States, 6/01/25.

Investigation of Aerodynamic Characteristics of a Generic Transport Aircraft in Ground Effect Using URANS Simulations @conference{37873127f2654751a6076eba6482930a, title = "Investigation of Aerodynamic Characteristics of a Generic Transport Aircraft in Ground Effect Using URANS Simulations", abstract = " This paper focuses on computational prediction of aerodynamic and the flow field characteristics for NASA Common Research Model (CRM) in it's High-Lift (HL) configuration in close proximity to the ground. The URANS simulation with the Spalart-Allmaras (SA) turbulence model is checked for the quality of the generated mesh and compared with the available wind tunnel data. The obtained simulation results in the immediate vicinity of the ground demonstrate significant changes in the longitudinal and lateral-directional aerodynamic characteristics in aircraft banked positions, which is important for a better understanding of aircraft landing in crosswind conditions. ", keywords = "physics, flu-dyn", author = "Mohamed Sereez and Nikolay Abramov and Mikhail Goman", note = "RAeS Applied Aerodynamics Conference 2022; RAeS Applied Aerodynamics Conference 2022 ; Conference date: 13-09-2022 Through 15-09-2022", year = "2022", month = oct, day = "2", language = "English", } . RAeS Applied Aerodynamics Conference 2022, 13/09/22.

CONFERENCE PAPER

Wing Rock Prediction in Free-to-Roll Motion Using CFD Simulations @inproceedings{5b68d8c517e34f29a6eed32698c7aaa8, title = "Wing Rock Prediction in Free-to-Roll Motion Using CFD Simulations", abstract = "The free-to-roll wing rock CFD simulation of a slender 80-degree delta wing is performed using the Dynamic Fluid-Body Interaction (DFBI) framework and the overlap/chimera mesh method. The purpose of the simulations carried out was to test the capabilities of the current CFD methods for predicting wing rock motion over a wide range of angles of attack, including strong conical vortex interactions and vortex breakdown phenomenon. The predictions of steady aerodynamic dependencies and the aerodynamic stability derivatives based on forced oscillation tests along with the time histories of the wing rock motion of an 80-degree delta wing are in good qualitative and quantitative agreement with the available wind tunnel experimental data demonstrating onset of the wing rock motion. At higher angles of attack with vortex breakdown CFD simulations demonstrated an excitation of the large amplitude regular oscillations or the low amplitude chaotic oscillations depending on the applied initial conditions.", author = "Mohamed Sereez and Caroline Lambert and Nikolay Abramov and Mikhail Goman", year = "2023", month = oct, day = "2", language = "English", booktitle = "10th EUCASS Conference", publisher = "European Conference for Aeronautics and Space Sciences", address = "Switzerland", note = "10th Aerospace Europe Conference : Joint 10th EUCASS-9th CEAS Conference ; Conference date: 09-07-2023 Through 13-07-2023", url = "https://eucass-ceas-2023.eu/", } . 10th EUCASS Conference.

DISSERTATION THESIS

(2018). Computational Prediction of Stall Aerodynamics and Evaluation of Ground Effect for a Generic Transport Aircraft .

MANUAL

(2016). Computational Simulation of Airfoils Stall Aerodynamics at Low Reynolds Numbers . Royal Aeronautical Soceity.