Issue |
Title |
File |
Vol 61, No 1 (2018) |
Sensitivity Algorithm as a Solution of an Inverse Strength Problem Applied to Thin-Walled Structures |
 (Eng)
|
Kostin V.A., Valitova N.L.
|
Vol 60, No 4 (2017) |
Safety Analysis of Helicopter Autorotation Landing Execution on Conditions of Providing Skid Landing Gear Static Strength |
 (Eng)
|
Ligai V.A., Nedel’ko D.V., Korotkov L.V.
|
Vol 60, No 4 (2017) |
Numerical Modeling of Helicopter Main Rotor Behavior near a Small-Scale Helideck by the Vortex Method |
 (Eng)
|
Aparinov A.A., Kritskii B.S., Setukha A.V.
|
Vol 60, No 4 (2017) |
Dynamic Stability of a Cylindrical Shell under Alternating Axial External Pressure |
 (Eng)
|
Bakulin V.N., Volkov E.N., Simonov A.I.
|
Vol 60, No 4 (2017) |
Research on Nonlinear Deformation and Stability of an Advanced Aircraft Fuselage Composite Section under Pure Bending |
 (Eng)
|
Belov V.K., Zheleznov L.P., Ognyanova T.S.
|
Vol 60, No 3 (2017) |
Drop test simulation for a helicopter tail landing gear |
 (Eng)
|
Podruzhin E.G., Zagidulin A.R.
|
Vol 60, No 2 (2017) |
Nonlinear deforming of laminated composite shells of revolution under finite deflections and normal’s rotation angles |
 (Eng)
|
Dmitriev V.G., Biryukov V.I., Egorova O.V., Zhavoronok S.I., Rabinskii L.N.
|
Vol 60, No 2 (2017) |
The influence of the noise field on parametric oscillations of flexible square plates |
 (Eng)
|
Krylova E.Y., Yakovleva T.V., Bazhenov V.G.
|
Vol 60, No 1 (2017) |
Dynamic behavior of wing leading edge assembly with thermal protection coating |
 (Eng)
|
Antuf’ev B.A.
|
Vol 60, No 1 (2017) |
Analytical and asymptotic solution of boundary value problems in the mechanics of deformed shells under concentrated loading |
 (Eng)
|
Bakulin V.N., Vinogradov Y.I.
|
Vol 60, No 1 (2017) |
Analysis of structural elements made of composite materials with defects |
 (Eng)
|
Kokurov A.M., Odintsev I.N.
|
Vol 60, No 1 (2017) |
Solution of the five-layer beam bending problem using the calculus of variation |
 (Eng)
|
Osadchii N.V., Shepel’ V.T.
|
Vol 60, No 1 (2017) |
Finite element modeling of operation for thin-walled open cross section bars to analyze plate-rod systems |
 (Eng)
|
Serpik I.N., Shvyryaev M.V.
|
Vol 60, No 1 (2017) |
Development of wireless strain-gauge measurement system for structural tests |
 (Eng)
|
Uvarov M.V., Naumov V.P.
|
Vol 59, No 4 (2016) |
Analysis of a beam with a crack under irregular cyclic load |
 (Eng)
|
Kayumov R.A., Mukhamedova I.Z., Tuisina E.B.
|
Vol 59, No 4 (2016) |
Development and verification of an analytic technique to determine the stiffness parameters of braided tubular parts |
 (Eng)
|
Samipur S.A., Danilov Y.S.
|
Vol 59, No 4 (2016) |
Thermally excited vibrations of aircraft structural elements |
 (Eng)
|
Starovoitov E.I., Leonenko D.V., Rabinskii L.N.
|
Vol 59, No 3 (2016) |
Stress–strain analysis of a thin-shell part of fuselage using a triangular finite element with lagrange multipliers |
 (Eng)
|
Klochkov Y.V., Nikolaev A.P., Vakhnina O.V., Kiseleva T.A.
|
Vol 59, No 3 (2016) |
Dynamics of a discretely reinforced cylindrical shell under live load |
 (Eng)
|
Antuf’ev B.A.
|
Vol 59, No 3 (2016) |
Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory |
 (Eng)
|
Gorelov A.V., Nikolaev E.I., Sidorov I.N.
|
Vol 59, No 2 (2016) |
Fuzzy logic rule as a method for making a design decision in rocketry development |
 (Eng)
|
Zezin V.G., Reshetnikov M.I.
|
Vol 59, No 1 (2016) |
Nonlinear bending and stability of circular plates under the liquid pressure and temperature |
 (Eng)
|
Ganeeva M.S., Moiseeva V.E., Skvortsova Z.V.
|
Vol 59, No 1 (2016) |
Development of the discrete vortex cylinders method for calculating the helicopter rotor induced velocity |
 (Eng)
|
Nikolaev E.I., Nikolaeva M.N.
|
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