From 10/2004 to 06/2009, Bachelor of Engineering
From 10/2009 to 06/2011, Master
From 10/2015 to 06/2018, Doctorate
From 08/2011 to Present, Research Scientist grade III
From 10/2010 to 05/2013, Clean Sky I- BLADE
Stress and strength analyses for a Airbus Laminar Wing Structure
From 07/2013 to 11/2015, Clean Sky I- Afetr Body Demonstrator
Stress and strength analyses for a Dassault Tail Cone mockup
From 10/2015 to 07/2018, ESA Euclid
Structural optimisation for thruster's brackets
Structures and Materials
C. Coman, I. Dima, C. Moisei, Comparative study between random vibration and linear static analysis using Miles method for thruster brackets in space structures. INCAS Bulletin vol. 9, no. 2, 2017.
C. Coman, Comparative study between 2D and 3D FEM techniques in single bolt, single lap, composite bolted joints for space structures. INCAS Bulletin vol. 9, no. 3, 2017.
C. Coman, Static and dynamic design methods for hybrid bolted joints in a satellite structure. INCAS Bulletin vol. 10, no. 2, 2018.
C. Coman, 'Geometry Effects on Failure Mechanisms of Hybrid Metal-Composite Bolted Joints', International Journal of Latest Research in Engineering and Technology, ISSN: 2454-5031(Online), Volume 04, No. 08, 2018, Page No. 34-51.
C. Coman, 'Thermal Effects on the Failure Mechanisms of Hybrid Metal-Composite Multi-Bolts Joints', International Journal of Recent Scientific Research, ISSN: 0976-3031(Online), Volume 9, No. 8 (C), 2018, Page No. 28407-28416.
C. Coman, Temperature effects on damage mechanisms of hybrid metal-composite bolted joints using SHM testing method, Proceeding in “The Seventh International Conference on Fatigue of Composites “, Vicenza, Italy, 4-6 July 2018.
I. Dima, C. Moisei, C. Coman, M. Nastase, C. Liliceanu, a. Petre, "Comparative study between random vibration and linear static analysis using Miles method for thruster brackets in space structures", the Fifth International Workshop on numerical Modelling in Aerospace Science, NMAS, Bucharest, Romania, 17-18 May 2017