05. Авиационная и ракетно-космическая техника
Aerodynamic substantiation of necessity of performance of the emergency landing at refusal of one and two engines out of airdrome without run
24.02.2020
1242
Aerodynamic justification and features of landing with one engine running on the helicopter "ANSAT-U"
17.12.2019
1233
Numerical simulation of fluidization in ANSYS Fluent
18.07.2019
1181
Mathematical modeling of the dynamic interaction of a solid with its surrounding space in the LS-Dyna software package
16.06.2019
1343
SHF devices non- destructive methods of control
16.04.2019
1527
To the question of mathematical modelling of the dual-mode rocket engine on solid fuel
19.09.2018
1345
The mathematical modeling of automatic aircraft landing TU-204SM in a broad range of expected operation conditions
13.05.2018
1705
Eexploration of the stress-deformed state of connections with reinforcein details from polymeric composite materials
16.06.2017
1919
Ensuring operational reliability of nano-electromechanical sensors of data management complexes of mobile objects: world outlook aspects
08.02.2017
1782
Project of a spacecraft propelled by electromagnetic fields
21.01.2017
4163
The impact of criterion numbers on the forces affecting on the aircraft in the high-enthalpy flow
18.09.2016
2219
Response test of wave processes in lineal regular systems
23.07.2015
2040
Influence of initial conditions on the rocket pods trajectory starting under water upon delivery of effective load in a present area
23.07.2015
2280