| Enhanced modeling of 3D composite preform deformations taking into account local fiber bending stiffness S Mathieu, N Hamila, F Bouillon, P Boisse Composites Science and Technology 117, 322-333, 2015 | 90 | 2015 |
| Data merging of AE sensors with different frequency resolution for the detection and identification of damage in oxide-based ceramic matrix composites N Guel, Z Hamam, N Godin, P Reynaud, O Caty, F Bouillon, A Paillassa Materials 13 (20), 4691, 2020 | 31 | 2020 |
| Accurate measurement of in-plane and out-of-plane shear moduli on 3D woven SiC-SiBC material N Tableau, Z Aboura, K Khellil, L Marcin, F Bouillon Composite Structures 172, 319-329, 2017 | 18 | 2017 |
| Method for making an acoustic absorption panel in particular for the nacelle of an aircraft engine LG Valleroy, F Bouillon US Patent 8,047,326, 2011 | 18 | 2011 |
| An efficient computational strategy of cycle-jumps dedicated to fatigue of composite structures O Sally, F Laurin, C Julien, R Desmorat, F Bouillon International Journal of Fatigue 135, 105500, 2020 | 13 | 2020 |
| Beam for a cascade thrust reverser A Bellanger, F Bouillon, L Dubois US Patent 9,341,142, 2016 | 12 | 2016 |
| Thrust reverser supporting structure including composite reinforcements and a base having an unclosed cross section A Bellanger, F Bouillon, L Dubois US Patent 9,409,650, 2016 | 9 | 2016 |
| Indicators for the damage evolution at intermediate temperature under air of a sic/[si-bc] composite subjected to cyclic and static loading E Racle, N Godin, P Reynaud, M R'Mili, G Fantozzi, L Marcin, F Bouillon, ... chez Mechanical Properties and Performance of Engineering Ceramics and …, 2014 | 9 | 2014 |
| Coupling system connecting an internal structure and an external stucture of a jet engine nacelle F Bouillon, P Dunleavy US Patent App. 12/673,259, 2011 | 9 | 2011 |
| Stub frame for a cascade thrust reverser structure A Bellanger, L Dubois, F Bouillon, S Bardin US Patent 8,840,064, 2014 | 6 | 2014 |
| Fatigue lifetime modeling of oxide/oxide composites O Sally, C Julien, F Laurin, R Desmorat, F Bouillon Procedia engineering 213, 797-803, 2018 | 5 | 2018 |
| Damage analysis in 3D woven SiC/SiC ceramic matrix composite B Legin1&2, Z Aboura, F Bouillon, S Denneulin Advances in High Temperature Ceramic Matrix Composites and Materials for …, 2017 | 5 | 2017 |
| Locking and stability of 3D woven composite reinforcements S Mathieu, P Boisse, N Hamila, F Bouillon Key Engineering Materials 611, 292-299, 2014 | 5 | 2014 |
| Bearing damage identification in oxide/oxide ceramic matrix composite with a new test design M Broutelle, F Lachaud, L Barrièrre, A Daidié, A Chardonneau, F Bouillon Composite Structures 236, 111902, 2020 | 4 | 2020 |
| Nacelle for an aircraft engine A Bellanger, F Bouillon, L Dubois US Patent 9,010,681, 2015 | 4 | 2015 |
| Experimental investigation of the in plane and through thickness shear damages on 3D woven CMC using multi-instrumented torsional tests N Tableau, K Khellil, Z Aboura, P Feissel, F Bouillon, L Marcin 16th Eur. Conf. Compos. Mater. ECCM 2014, 22-26, 2014 | 4 | 2014 |
| Acoustic treatment structure for an aircraft propulsion unit nacelle F Bouillon, F Dupe, B Carrere, B Desjoyeaux US Patent 11,512,666, 2022 | 3 | 2022 |
| Method for detecting the presence of bubbles during operations of injecting resin for the manufacture of fibre composite components F Bouillon, J Breard, L Bizet, S Gueroult US Patent App. 14/285,894, 2014 | 3 | 2014 |
| Leading edge structure, in particular for the air intake of the nacelle of an aircraft engine F Bouillon, F Ravailler US Patent App. 13/383,651, 2012 | 3 | 2012 |
| Cell structure and acoustic attenuation device for a nacelle of an aircraft propulsion assembly B Desjoyeaux, DS De Vasconcellos, F Bouillon, A DELEHOUZE US Patent 11,427,299, 2022 | 2 | 2022 |
