Department of Aeronautical Engineering

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About Department of Aeronautical Engineering

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17

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18

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380

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487

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Who works at the Department of Aeronautical Engineering

Department of Aeronautical Engineering has more than 18 academic staff members

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Prof.Dr. ali mohammed Emhammed almabrok
Department of Aeronautical Engineering - faculty of Engineering
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Mr. Ahmad Abdussalam Mohamed Almkhlufi
Department of Aeronautical Engineering - faculty of Engineering
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Prof.Dr. Saleh Ramadan Gashoot Abdussalam
Department of Aeronautical Engineering - faculty of Engineering
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Prof.Dr. Gamal Mohamed Ali Ashawesh
Department of Aeronautical Engineering - faculty of Engineering
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Mr. Ahmad Abdussalam Mohamed Almkhlufi

التعليم والمؤهلات:
• بكالوريوس الهندسة من كلية الهندسة – جامعة طرابلس.
• ماجستير الهندسة من كلية الهندسة – جامعة طرابلس.

البحوث المنشورة:

1. “The development of engineering education to meet the needs of the community”, Saleh R. Gashoot and Ahmad A. Al-Makhloufi, Third forum on engineering education, Building partnership with government, industry and society, Sharjah, United Arab Emirates, 14-15 October 2003. [In Arabic Language].
2. “Studying the effect of the shape on the performance of the Darrieus rotor”, Ali M. Elmabrok and Ahmad A. Al-Makhlufi, World renewable energy and environment conference (2006 Tripoli-Libya)
3. “Evaluation of Fuzzy Model Reference Learning Control for Yaw angle control”, Ahmad A. Makhlufi, Abdulhamid A. Ghmmam, and ATahir EL Hashan, International ICASAT2007 conference, Tripoli-Libya, Apr. 2007.
4. “Buckling of plates on a foundation with different types of sides support”, Dr. Ali N. Suri, Ahmad A. Al-Makhlufi, ICMAE 2013: International Conference on Mechanical and Aerospace Engineering, Bangkok, Thailand, December, 24-25, 2013.
5. “Local buckling of web-core and foam-core sandwich panels”, Dr. Ali N. Suri, Ahmad A. Al-Makhlufi, ICAMAME 2014: XII International Conference on Aerospace, Mechanical, Automotive and Materials Engineering, Dubai, UAE, April, 8-9, 2014.
6. “Aircraft Motion Simulation in Time Domain- A Useful Tool in Flight Mechanics”, Abdulhamid A. Ghmmam and Ahmed A. Makhlufi, ICEER2014-McMaster; International Conference on Engineering Education and Research, Hamilton, Canada, August 24-26, 2014.
7. Abdulhamid A. Ghmmam, Saad E. Issa and Ahmed A. Makhlufi, “Training Aircraft Design and Development Program: Towards Technology Transfer”, International Conference on Mechanical and Aerospace Engineering; ICMAE 2017, Toronto, Canada, May 29-30, 2017.

Publications

Some of publications in Department of Aeronautical Engineering

Aerodynamic design and performance estimation of horizontal-axis wind turbine

Abstract Estimation of wind characteristics is considered as the first essential step to evaluate a wind energy project based on information about all aspects of the implementation and operation of the project. It's therefore necessary to have detailed knowledge of the wind to design a suitable wind turbine for a certain zone and also to estimate its performance accurately. The first step in this thesis is study the wind energy and wind assessment in the selected site (Zuara) based on the available wind data, which are obtained from the representative meteorological station. The second step in this thesis is study is to design a suitable horizontal axis wind turbine. Design (HAWT) to achieve satisfactory levels of performance starts with knowledge of the aerodynamic forces acting on the blades. The blade element momentum theory (BEM) is applied for HAWT blade design and to predict the performance of the rotor. A computer program for HAWT blade design and its performance analysis is belt. The input of this program is: power required from a turbine, number of blades, design wind velocity, design tip-speed ratio and properties of the selected airfoil. While the output are: blade geometry parameters (chord and twist distribution), power, torque and thrust coefficients versus tip-speed ratios. This study indicates that capacity factor on the Zuara site equal 3 and it is seen that possible to designed wind turbine to extracting the power from the wind with satisfactory levels of performance in the selected site
فرج الأخضر شنشن (2014)
Publisher's website

INFLUENCE OF GEOMETRICAL VARIABLES OF DARRIEUS ROTOR ON ITS PERFORMANCE

تتسم المروحة الهوائية من النوع المعروف بإسم Darrieus بمميزات من بينها البساطة في تصميم الدوار و موقع المُولِّد فضلا عن البساطة في تصميم أي منظومة تحكم تحتاجها. و حيث أن الدوار يعتبر المسؤول الرئيس على إستخلاص طاقة الحركة الكامنة في الريح، عليه فإنه من المنتظر بكل تأكيد أن يكون لخصائص الشكل الهندسي لهذا الدوار أثر ملحوظ على أدائه و بالتالي على أداء المروحة بوجه عام. وقد تم في إطار هذه الرسالة دراسة تأثير خصائص الشكل التالية: عدد ريش الدوار، نسبة وتر الريشة إلى نصف قطر الدوار، نسبة الصلادة، و نسبة إرتفاع الدوار إلى قطره. كما تم أيضا دراسة تأثير قيمة رقم رينولدز على أداء الدوار. أسِّست الدراسة على إستخدام نموذج رياضي يدعى "Multiple Streamtube" و مقطع ريشة من نوع "NACA0012" كما أعدت النتائج النهائية في هيئة مخططات بيانية توضح كلا من معامل العزم و معامل القدرة كدالة فيما يسمى بالسرعة الطرفية النسبية. Abstract Darrieus wind turbines offer a number of advantages such as simplicity of design of structure, generator, and any control system. With the rotor being the direct means of extracting kinetic energy from the wind, its particular geometry must undoubtedly have a great effect on the overall performance of the turbine. The rotor geometrical parameters investigated in this study were: number of blades, chord to radius ratio, solidity, height to radius ratio. Moreover, the effects of Reynolds number were also included. The analysis was based on the use of a multi streamtube model and NACA0012 rotor-blade profile. Results are presented in the form of power and torque coefficients as functions of tip-speed ratio.
هشام إبراهيم أبوسنوقة (2010)
Publisher's website

Free vibration analysis of a composite wing box-initial aerodynamic investigations

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Saleh R. Abdussalam Gashoot, J. M. Ashawesh, Ali M. Elmabrouk(4-2004)
Publisher's website
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