| Issue |
Section |
Title |
File |
| Vol 3, No 1 (2004) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Proving theorems of changing structure rigidity |
(Rus)
|
| Vol 5, No 1 (2006) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Optimization of a thin-walled wireframe structure with strength and stiffness limitations |
(Rus)
|
| Vol 5, No 1 (2006) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Optimal positioning of supports for statically definable beams |
(Rus)
|
| Vol 8, No 1 (2009) |
CONTROL, COMPUTER SCIENCE AND INFORMATION SCIENCE |
Comparative analysis of different approaches to designing thin-walled element structures of composite materials |
(Rus)
|
| Vol 9, No 4 (2010) |
CONTROL, COMPUTER SCIENCE AND INFORMATION SCIENCE |
Model for the estimation of design work acceleration by parallelization of iterative process in research-intensive mechanical engineering |
(Rus)
|
| Vol 11, No 1 (2012) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
High fidelity modeling at early stages of airframe structural design |
(Rus)
|
| Vol 14, No 2 (2015) |
MECHANICAL ENGINEERING AND POWER ENGINEERING |
Numerical and experimental study of the strength of fabric carbon-epoxy composite structures |
(Rus)
|
| Vol 17, No 1 (2018) |
MECHANICAL ENGINEERING |
Сhoice of materials for producing dimensionally stable load-carrying structures |
(Rus)
|
| Vol 17, No 1 (2018) |
MECHANICAL ENGINEERING |
Topology optimization of a load-bearing structure via the method of convex linearization |
(Rus)
|
| Vol 1, No 1 (2002) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Estimation of weight efficiency of the power schemes of lift surfaces |
(Rus)
|
| Vol 2, No 1 (2003) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
STRUCTURE STIFFENING BY TOPOLOGICAL CHANGES |
(Rus)
|
| Vol 19, No 3 (2020) |
MECHANICAL ENGINEERING |
Optimization of honeycomb sandwich floor panels made of polymer-matrix low-combustible composite materials based on high-strength carbon and glass fibers and adhesive binder |
(Rus)
|
| Vol 20, No 1 (2021) |
MECHANICAL ENGINEERING |
Digital design of heat-resistant dimensionally stable carbon laminate (CFRP) structures |
(Rus)
|
| Vol 20, No 2 (2021) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Optimal design of sandwich floor panels made of high-strength composite materials considering stiffness constraints |
(Rus)
|
| Vol 21, No 2 (2022) |
MECHANICAL ENGINEERING |
Experimental and analytical determination of the elastic characteristics of layered woven composites |
(Rus)
|
| Vol 22, No 3 (2023) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Determining aerodynamic characteristics of small unmanned aerial vehicles involving flight experiment |
(Rus)
|
| Vol 23, No 1 (2024) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Reducing energy consumption of vertical take-off and landing unmanned aerial vehicle using hybrid technical solutions |
(Rus)
|
| Vol 23, No 1 (2024) |
MECHANICAL ENGINEERING |
Effective volume of short carbon fibers in a composite from chopped thin tapes |
(Rus)
|
| Vol 23, No 3 (2024) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Automation of conceptual design and modification of aircraft type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 1: Methods and models |
(Rus)
|
