Issue |
Title |
No 4 (2021) |
© ПНИПУ Numerical and experimental research of the evaluation of the mechanical behavior of carbon fiber reinforced polymerspecimens with an embedded Smart-layer |
|
Baranov M.A., Nikiforov A.S., Mikryukov A.O., Ermakov D.A. |
No 1 (2017) |
Numerical and experimental study of composite bulkhead partition strength with in-situ x-ray monitoring |
|
Potrahov N.N., Anoshkin A.N., Zuiko V.Y., Osokin V.M., Pisarev P.V., Pelenev K.A. |
No 4 (2021) |
Simultaneous identification of mechanical properties of functionally graded plates under the Kirchhoff and Tymoshenko models |
|
Bogachev I.V. |
No 3 (2021) |
The Applied mechanical and mathematical model of grinding of a solid particle by static crushing |
|
Guryanov G.A., Abdeev B.M., Baigereyev S.R., Kim V.A., Suleimenov A.D. |
No 1 (2021) |
The analysis of flutter characteristics based on generalized parameters of eigen modes of vibrations |
|
Barinova K.I., Dolgopolov A.V., Orlova O.A., Pronin M.A. |
No 4 (2020) |
Study Smart-layer effect on the physical and mechanical characteristics of the samples from polymer composite materials under quasi-static loading |
|
Shipunov G.S., Baranov M.A., Nikiforov A.S., Golovin D.V., Tihonova A.A. |
No 2 (2013) |
Effect of stiffness loading system on the equilibrium of the crack growth under quasi-static loading |
|
Bazhukov P.S., Vildeman V.E., Ilinyh A.V., Tretyakov M.P. |
No 4 (2014) |
Technologies and problems of composite materials mechanics for production of outlet guide vane for aircraft jet engine |
|
Anoshkin A.N., Zuiko V.Y., Shipunov G.S., Tretyakov A.A. |
No 4 (2015) |
Stress-strain analysis and strength prediction of composite outlet guide vane for aircraft jet engine |
|
Grinev M.A., Anoshkin A.N., Pisarev P.V., Zuiko V.Y., Shipunov G.S. |
No 3 (2024) |
EXPERIMENTAL VERIFICATION OF THE FREQUENCY METHOD FOR EVALUATING THE AXIAL LOAD AND IMPERFECTION OF BOUNDARY CONDITIONS IN REINFORCING BARS |
|
Azarov A.A., Popov A.L. |
No 3 (2015) |
CAD/CAE modelling of mechanical behavior of composite outlet guide vane for aircraft jet engine |
|
Grinev M.A., Anoshkin A.N., Pisarev P.V., Zuiko V.Y., Shipunov G.S. |
No 6 (2023) |
FATIGUE SENSITIVITY OF GFRP UNDER PROPORTIONAL CYCLIC TENSION WITH TORSION |
|
Wildemann V.E., Staroverov O.A., Mugatarov A.I., Kuchukov A.M. |
No 4 (2016) |
Experimental and numerical research of the dynamic response of composite outlet guide vane for aircraft jet engine |
|
Grinev M.A., Anoshkin A.N., Pisarev P.V., Shipunov G.S., Nikhamkin M.S., Balakirev A.A., Konev I.P., Golovkin A.Y. |
No 4 (2022) |
SIMULATION OF VIBRATORY PLATE INTERACTION WITH THE GROUND SURFACE |
|
Tyuremnov I.S., Efimov S.S. |
No 2 (2016) |
Manufacturing defects in composite flanges: modelling and analysis of influence on static strength |
|
Anoshkin A.N., Zuiko V.Y., Osokin V.M., Tretyakov A.A., Pisarev P.V. |
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