قسم هندسة الطيران

المزيد ...

حول قسم هندسة الطيران

أُنشئ قسم هندسة الطيران مع بداية السنة الدراسية 1975-1976م كجزء من الكلية للقيام بتأهيل المهندسين في مجالات هندسة الطيران بهدف الاعتماد على العناصر الوطنية في هذا المجال التقني المتقدم، ويتولى تسيير البرنامج العلمي والبحثي بالقسم أكثر من 20 عضو هيئة تدريس في تخصصات مختلفة.

حقائق حول قسم هندسة الطيران

نفتخر بما نقدمه للمجتمع والعالم

17

المنشورات العلمية

18

هيئة التدريس

380

الطلبة

487

الخريجون

البرامج الدراسية

بكاليوريوس هندسة الطيران
تخصص هندسة الطيران

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التفاصيل
ماجستير هندسة الطيران
تخصص هندسة الطيران

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التفاصيل

من يعمل بـقسم هندسة الطيران

يوجد بـقسم هندسة الطيران أكثر من 18 عضو هيئة تدريس

staff photo

أ. أحمد عبدالسلام محمد المخلوفي

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.

منشورات مختارة

بعض المنشورات التي تم نشرها في قسم هندسة الطيران

Aeroelastic Analysis of a Real Metal Wing Box with Varying Root Stiffness

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saleh R. Abdussalam Gashoot, Gamal M. Ashawesh , M. Kaheal(2-2005)
Publisher's website

characteristics of crack tip in elastic zone in an isotropic media

not exist
Saleh R. Abdussalam Gashoot, M.L.Ayari, Yi, Z. (6-1997)
Publisher's website

Influence of Design Tip Speed Ratio and Rated Wind Speed on Energy Yield of Horizontal Axis Wind Turbine

Abstract Wind turbines are the means of converting wind energy into electrical energy. It is not unexpected that certain brands of horizontal wind turbines are optimally designed for certain wind speed regimes prevailing at certain sites. It has been the objective of this study to find out whether it is possible to design a wind turbine that is more suitable for a site of lower annual mean wind speed such as the western coast of Libya. In achieving this objective, use was made of a typical wind turbine aerodynamic design and performance analysis procedure together with actual wind speed data recorded at the city of Misurata.Based on the annual wind energy yield obtained from different designs of wind turbines having different rated wind speeds and different blade design tip speed ratios, this study indicates that the decrease of the rated wind speed leads to a continuous increase of annual energy yield as well as an increase of the cost of the wind turbine. Therefore the optimum value of rated wind speed for this site may only be determined as a compromise between added wind energy yield and added cost. Moreover, for any given rated wind speed this study indicates that a blade design tip speed ratio equal to six seems to be the optimum value for the given site.
محمد على نايلي (2015)
Publisher's website