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Saad Theeyab Faris
Saad Theeyab Faris
Verified email at uodiyala.edu.iq
Title
Cited by
Cited by
Year
Development and properties of fiber metal laminate used in aircraft wing by using epoxy-novolac
AM Kadhum, ST Faris, AA Al-katawy
IOP Conference Series: Materials Science and Engineering 518 (3), 032034, 2019
92019
Cumulative fatigue damage of AA7075-T6 under shot peening and ultrasonic surface treatments
MS Mahammed, HJ Alalkawi, ST Faris
Diyala Journal of Engineering Sciences, 1-10, 2021
62021
Study of The Stress and Strain Distribution During Deep Drawing and Ironing Process of Metals with A Circular Profiled Die.
ST Faris
Diyala Journal of Engineering Sciences, ISSN 8716, 80-95, 1999
61999
Analysis of Plane Strain Rolling Rigid Plasttic Materials Using Finite Element Method
ST Faris
Diyala Journal of Engineering Sciences, 99-115, 2015
42015
Improvement of the Mechanical Characteristics of Fiber Metal Laminate (FMLs) Used for Aircraft Wing Using Epoxy-Resole
ST Faris, AA Al-katawy, AM Kadhum
Diyala Journal of Engineering Sciences, 79-89, 2021
32021
Combine shot penning (SP) and ultrasonic impact treatment (UIT) for soil corrosion buckling strength enhancement of AA 2014-T4
HJM Al-Alkawi, ST Faris, SN Naji
Al-Nahrain J Eng Sci 23 (2), 144-52, 2020
32020
Improving the mechanical properties of fiber metal laminate composite used in aircraft wing
AM Kadum, AA Al-katawy, ST Faris, EE Kader
Al-Nahrain Journal for Engineering Sciences 22 (1), 9-13, 2019
32019
Improvement and Properties of Fiber Metal Laminates Used in Aircraft Wing by Using Graphite-Polyester
AM Kadhum, ST Faris, AA Al-katawy
University of Diyala–College of Engineering, 2019
32019
Prediction of Cutting Tool Performance With Double Rake Geometry Using Finite Element Technique
ST Faris
journal of engineering and applied sciences, 2018
32018
Cracks length OF AA7075 measurement under electrical potential drop technique
MS Mahammed, ST Faris
J. Mech. Eng. Res. Dev 44, 158-169, 2021
22021
Mechanical properties and fatigue life evalution under high temperature and shot peening application using AA7001-T6
HS Mahdi, HJM Alalkawi, ST Faris
IJNea M 16 (3), 13, 2023
12023
EVALUATION OF CREEP-FATIGUE LIFE AND STRENGTH FOR AA7001-T6 UNDER CONSTANT AMPLITUDE LOADING.
HS Mahdi, HJ Alalkawi, MT Mohamed, ST Faris
Eastern-European Journal of Enterprise Technologies 118 (12), 2022
12022
Study and Design the Hydrodynamic Deep Drawing Process for Blanks of Non Uniform Thickness
S Faris
Diyala Journal of Engineering Sciences, 40-56, 2010
12010
investigation of some parameters influencing of three dimensional tube extrusion process of ellipse section through streamline die
ST Faris, EE Kader
Diyala Journal of Engineering Sciences, 1-15, 2010
12010
Crack Growth Model for Evaluation the Fatigue Life of Aluminum Alloys
ZM Chaloob, ST Faris, HJM Al Alkawi, AH Mohamed
Diyala Journal of Engineering Sciences, 128-141, 2023
2023
Cumulative Fatigue Life Estimation Under Combined Shot Peening and Elevated Temperature for AA7001-T6
HS Mahdi, ST Faris, RM Abed, HM Alalkawi, R Nasir
Diyala Journal of Engineering Sciences, 50-59, 2023
2023
RETRACTED: ALLOCATION OF HYBRID COMPOSITE MATERIALS IN FRICTION DISC CLUTCHES
IM Naemah, ST Faris, KN Abed
Journal of Engineering and Sustainable Development 27 (3), 350-362, 2023
2023
Improving the Mechanical Properties of a Composite material Reinforced with Glass Carbon for Aircraft Application
K Abed, S Faris, I Naemah
Al-Nahrain Journal for Engineering Sciences 26 (1), 1-6, 2023
2023
ALLOCATION OF HYBRID COMPOSITE MATERIALS IN FRICTION DISC CLUTCHES
IM Naemah, ST Faris, KN Abed
Journal of Engineering and Sustainable Development (JEASD) 27 (3), 2023
2023
Studying and Improving the Hardness Properties of Gray Cast Iron
ST Faris, HS Mahdi, KN Abed
Diyala Journal of Engineering Sciences, 114-121, 2022
2022
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