Iraq Engineering Society- Babel

Aircraft Design
Gas Dynamics
Aerodynamics
Mechanical Vibrations
Mathematics
Engineering and Numerical Analysis
Strength of Materials
Damage Modeling in Composite Materials (Fiberglass, Carbon Fiber, and Metal Reinforced Composite)
Failure Analysis
Buckling Analysis
Modeling and Analysis of Mechanical and Thermal Stresses of Structures Made of Composite Materials and Metals

Courses

1- Using finite element programs in modeling and designing engineering structures

2- Using the program
EndNote
in organizing references in scientific research and theses

Workshopes

1-

Third Workshop on Physics Enhancing Machine Learning: mechanics and materials (27/11/2024)

Seminars

1-

"Remark and Correct Alliance: The optimal solution for performing and correcting assessment tests in Iraqi universities"

Journal papers  Nawras H. Mostafa, S.O. Waheed, Ahmad S.M. Al-Azzawi, Optimum Design of Symmetric Laminated Reinforced Plate Subjected to in-Plane Compressive Loading: Buckling Analysis, Article , August 2009.  Salam Hadi Hussain, Mohammed Yousif Jabbar, Ahmad Saddy Mohamad, Influence of presence of inclined centered baffle and corrugation frequency on natural convection heat transfer flow of air inside a square enclosure with corrugated side walls. International Journal of Thermal Sciences, Pages 1799- 1808, 2011.  Ahmad S.M. Al-Azzawi, Numerical Investigation of Free Vibration on New Stepped Wing Model. Article, January 2012.  Ahmad S.M. Al-Azzawi, J.P. McCrory, L.F. Kawashita, C.A. Featherston, R. Pullin, K.M. Holford. Buckling and Post-Buckling Behaviour of Glare Laminates Containing Splices and Doublers. Part1: Instrumented tests, Composite Structures 2017.  Ahmad S.M. Al-Azzawi, L.F. Kawashita, C.A. Featherston. Buckling and PostBuckling Behaviour of Glare Laminates Containing Splices and Doublers. Part2: Numerical Modelling, Composite Structures 2017.  Ahmad S.M. Al-Azzawi, L.F. Kawashita, C.A. Featherston, A modified cohesive zone model for fatigue delamination in adhesive joints: Numerical and experimental investigations, Composite Structures, Volume 225, 2019, 111114, https://doi.org/10.1016/j.compstruct.2019.111114.  Al-Azzawi AS, Kawashita LF, Featherston CA. Predicting interlaminar damage behaviour of fibre-metal laminates containing adhesive joints under bending loads. Journal of Reinforced Plastics and Composites. 2022; 41(5-6):167-186, https://doi:10.1177/07316844211051706.  Ahmad S.M. Al-Azzawi, John McCrory, Zhangming Wu, Carol A. Featherston, A novel semi-analytical approach for predicting the buckling and Postbuckling behaviour of Glare fibre metal laminates, Thin-Walled Structures, Volume 181, 2022,109987, https://doi.org/10.1016/j.tws.2022.109987.  Ahmad S.M. Al-Azzawi, C.A. Featherston, Colin Lupton, Chulin Jiang, Antigoni Barouni, Ugur Koklu, Khaled Giasin, Impact characteristics of S2-glass fibre/FM94-epoxy composites under high and cryogenic temperatures: experimental and numerical investigation, Composites Part B: Engineering, 2024, 111786, ISSN 1359-8368, https://doi.org/10.1016/j.compositesb.2024.111786. Conference papers  Ahmad S.M. Al-Azzawi, J.P. McCrory, L.F. Kawashita, C.A. Featherston, R. Pullin, K.M. Holford. Delamination Characteristics Of Splices And Doublers In Glare Laminates During Buckling, In 11th World Congress On Computational Mechanics (WCCM XI). July 20 - 25, 2014: Barcelona, Spain.  Ahmad S.M. Al-Azzawi, J.P. McCrory, L.F. Kawashita, C.A. Featherston, R. Pullin, K.M. Holford. Buckling And Postbuckling Behaviour Of Glare Laminates Containing Splices And Doublers: Experimental And Numerical Investigations, in 3rd Int. Conference on Buckling and Postbuckling Behaviour of Composite Laminated Shell Structures. 25-27 March 2015: Braunschweig, Germany.  Ahmad S.M. Al-Azzawi, L.F. Kawashita, C.A. Featherston. Delamination Characteristics Of Glare Laminates Containing Doubler And Splice Features Under High Cycle Fatigue Loading, in the 24th UK Conference of the Association for Computational Mechanics in Engineering. 31 March – 01 April 2016: Cardiff University, UK.  Ahmad S.M. Al-Azzawi, L.F. Kawashita, C.A. Featherston. The effect of circular delaminations on the buckling and postbuckling behaviour of Glare laminates under compression, in the 11th Int. Conference of Advances in Experimental Mechanics. 5-7 September 2016: University of Exeter, UK.  Ahmad S.M. Al-Azzawi, L.F. Kawashita, C.A. Featherston. A constitutive model for elastic-plastic behaviour and delamination damage in fibre metal laminates, Proceedings of the 25th UKACM Conference on Computational Mechanics, 12 –13 April 2017, University of Birmingham, United Kingdom.  Ahmad S.M. Al-Azzawi, L.F. Kawashita, C.A. Featherston. Modelling Fatigue Damage in Fibre Metal Laminate Adhesive Joints, 21st International Conference on composite Materials (ICCM-21) in Xi’an, China, 20-25 August 2017.  Ahmad S.M. Al-Azzawi, Muthana Al-Saymaree, L.F. Kawashita, C.A. Featherston. Quasi-static damage in Fibre Metal Laminate Adhesive Joints: Experimental Investigations, 20th International Conference on Composite Structures (ICCS-20), Paris, France, 4-7 September 2017.  Ahmad S.M. Al-Azzawi, J.P. McCrory, L.F. Kawashita, C.A. Featherston, R. Pullin, K.M. Holford. Damage – Diagnosis and Prognosis in Fibre Metal Laminates for the Aerospace Industry Conference: IMEE-Innovation in Material for Extreme Environment, University of Huddersfield, Huddersfield, UK, 22-24th November 2017

Aircraft Design

Aircraft Structures

Gas Dynamics

Aerodynamics

Mechanical Vibrations

Mathematics

Engineering and Numerical Analysis

Fundamentals of Aviation

Engineering Drawing