Skvorcov, Yuriy V.

2023

• 1 Evtushenko M.A., Skvortsov Y.V., Khnyryova E.S. Estimation of Composites Delamination due to the Edge Effect // Advances in Transdisciplinary Engineering. — 2023. — Vol. 40. — P. 12-17

2022

• 1 Skvortsov Yu.V., Evtushenko M.A., Khnyryova E.S. Investigation of the Edge Effect in Laminated Composites Using the ANSYS Software // Journal of Aeronautics, Astronautics and Aviation 2022. — Vol. 54. Issue 4. № 4. — P. 421-432

2019

• 1 Chernyakin S.A., Perov S. N. , Skvortsov Y.V. Finite element modeling of conical lattice bays // Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019. — 2019. — P. 7-11

2018

• 1 Chernyakin S., Perov S. N. , Skvortsov Y. Numerical modeling of composite support for high-precision equipment // AIP Conference Proceedings. — 2018. — Vol. 2046.
• 2 Chernyakin S., Perov S. N. , Skvortsov Y. etc. The size stability of the primary structure of a small spacecraft // AIP Conference Proceedings. — 2018. — Vol. 2046.
• 3 Chernyakin S., Perov S. N. , Skvortsov Y. Probabilistic approach at delamination propagation problem in composite materials // AIP Conference Proceedings. — 2018. — Vol. 2046.

2017

• 1 Glushkov S.V., Skvortsov Yu.V., Perov S. N. etc. Finite element analysis of panels with surface cracks // AIP Conference Proceedings. — 2017. — Vol. 1798.
• 2 Aistov A.I., Skvortsov Yu.V., Chernyakin S.A. etc. Fatigue life prediction for expansion bellows // AIP Conference Proceedings. — 2017. — Vol. 1798.
• 3 Skvortsov Yu.V., Glushkov S.V., Aistov A.I. Research on the Low-cycle Structural Strength of the Fuel Tank Membrane // Procedia Engineering. — 2017. — Vol. 185. — P. 110-118
• 4 Skvortsov Yu.V., Glushkov S.V., Chernyakin S.A. Space Factors Influence on the Size Stability of Small Spacecraft Structure Elements // Procedia Engineering. — 2017. — Vol. 185. — P. 105-109
• 5 Chernyakin S.A., Skvortsov Yu.V., Perov S. N. Modelling of delamination growth in laminated plates using cohesive zone model techniques // AIP Conference Proceedings. — 2017. — Vol. 1798.

2016

• 1 Skvortsov Y.V., Chernyakin S.A., Glushkov S.V. etc. Simulation of fatigue delamination growth in composite laminates under mode I loading // Applied Mathematical Modelling 2016. — Vol. 40. Issue 15-16. — P. 7216-7224
• 2 Glushkov S.V., Skvortsov Y.V., Perov S. N. Probabilistic reliability of pipelines with surface cracks // 2016 5th International Conference on Reliability, Infocom Technologies and Optimization, ICRITO 2016: Trends and Future Directions. — 2016. — P. 145-150

2015

• 1 Skvortsov Y., Chernyakin S.A., Glushkov S.V. etc. Simulation of fatigue delamination growth in composite laminates under mode I loading // Applied Mathematical Modelling 2015. —
• 2 Chernyakin S., Skvortsov Y., Perov S. N. Failure analysis of thin-walled structure with delaminations // RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies. — 2015. — P. 17-20
• 3 Skvortsov Yu.V., Chernyakin S.A., Glushkov S.V. etc. Finite Element Modeling of Delamination Propagation in Composite Laminates // Applied Mechanics and Materials 2015. — № Vol. 756. — P. 347-352

2014

• 1 Glushkov S.V., Skvortsov Y.V. Fracture mechanics analysis of cylindrical panels with non-through cracks // Russian Aeronautics 2014. — Vol. 57. Issue 3. — P. 240-244
• 2 Glushkov S.V., Skvortsov Y.V., Perov S. N. Comparison of the results of solving the problem of fracture mechanics for pipe with non-through crack // PNRPU Mechanics Bulletin 2014. — Vol. 2014. Issue 3. — P. 36-49

2001

• 1 Aistov A.G., Leonov V.I., Savel'ev L.M. etc. Experience in work with Rebis AutoPIPE program at 'Giprovostokneft'' company // Gazovaya Promyshlennost 2001. — Issue 11. — P. 64-66

1993

• 1 Skvortsov Yu.V., Khazanov Kh.S. Nonlinear finite element of an arbitrary beam // Izvestiya Vysshikh Uchebnykh Zavedenij. Aviatsionnaya Tekhnika 1993. — Issue 1. — P. 9

1989

• 1 Skvortsov Yu.V., Khazanov Kh.S. Nonlinear analysis of arbitrary shell structures with use of a curvilenear isoparametric element // Sov Aeronaut 1989. — Vol. 32. Issue 2. — P. 14-17