| Mechanical characteristics evaluation of a single ply and multi-ply carbon fiber-reinforced plastic subjected to tensile and bending loads A Hadăr, F Baciu, AD Voicu, D Vlăsceanu, DI Tudose, C Adetu Polymers 14 (15), 3213, 2022 | 18 | 2022 |
| Benefits of 3D printing technologies for aerospace lattice structures. AD VOICU, A Hadăr, D Vlăsceanu Scientific Bulletin'Mircea cel Batran'Naval Academy 24 (1), 2021 | 15 | 2021 |
| Vibrational Study of a Helicopter Tail Rotor Blade with Different Polymer Inner Core Materials AD Voicu, A Hadăr, D Vlăsceanu, DI Tudose Mat. Plast 57, 169-178, 2020 | 6 | 2020 |
| A novel composite helicopter tail rotor blade with enhanced mechanical properties A Hadăr, AD Voicu, F Baciu, D Vlăsceanu, DI Tudose, ŞD Pastramă Aerospace 10 (7), 647, 2023 | 5 | 2023 |
| Improving the mechanical behavior of a helicopter tail rotor blade through the use of polyurethane foams AD Voicu, A Hadar, D Vlasceanu Revista de chimie 70 (11), 4123-4127, 2019 | 5 | 2019 |
| Validation of a numerical fluid flow analysis for a helicopter tail rotor blade using a subsonic wind tunnel AD Voicu, A Hadăr, D Vlăsceanu Macromolecular Symposia 389 (1), 1900099, 2020 | 4 | 2020 |
| Ballistic protection plates for military helicopters structures: Experimental and numerical research C Adetu, A Hadar, V Nastasescu, AE Adetu, AD Voicu, SD Pastrama Materials Today: Proceedings 93, 618-624, 2023 | 3 | 2023 |
| SHM Monitoring Methods and Sensors with Applications to Composite Helicopter Blades: A Review AD Voicu, A Hadăr, D Vlăsceanu, ŞD Pastramă Acta Universitatis Cibiniensis. Technical Series 72 (1), 1-11, 2020 | 3 | 2020 |
| Experimental and Numerical Analysis of Chlorinated Polyethylene Honeycomb Mechanical Performance as Opposed to an Aluminum Alloy Design F Baciu, A Hadăr, AD Voicu, D Vlăsceanu, DI Tudose Materials 15 (22), 8034, 2022 | 2 | 2022 |
| RESEARCH OF THE RICOCHET PHENOMENON APPEARING AT THE IMPACT BETWEEN A KINETIC PROJECTILE AND A PLATE C ADETU, A HADĂR, V NĂSTĂSESCU, AE ADETU, AD VOICU | | |
| ASPECTS REGARDING INTERLAMINAR STRESS DISTRIBUTION ON THE COMPOSITE LAMINATED SKIN OF A TAIL ROTOR BLADE EXPOSED TO AERODYNAMIC FORCES AD VOICU, A HADĂR, D VLĂSCEANU | | |
