On the Possibility of Increasing Rocky Target Penetration Depth for Compound Penetrators Featuring a Tail Assembly Jettisoned at Impact
| Authors: Fedorov S.V., Veldanov V.A., Fedorova N.A. | Published: 17.02.2019 |
| Published in issue: #1(124)/2019 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: high-speed penetration, rocky ground target, penetrator, penetrating unit, ballast mass jettisoning, recoil impulse | |
Accounting for Nonlinear Ship Motion in Navigational al Support of Submarine Ballistic Missile Launches
| Authors: Antsev G.V., Lysenko L.N., Petrov V.A. | Published: 22.04.2019 |
| Published in issue: #2(125)/2019 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: nonlinear ship motion models, optimum filtering, ballistic missile, submarine, inertial navigation system, pre-launch sequence, using velocity to determine initial conditions | |
Investigation of Throttling Characteristics in Supersonic Polyclinic Inlet
| Authors: Vnuchkov D.A., Zvegintsev V.I., Nalivaychenko D.G. | Published: 22.04.2019 |
| Published in issue: #2(125)/2019 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
| Keywords: multi-wedge air inlet, throttling characteristics, aerodynamic experiment, numerical simulation | |
Investigating the Specifics of Work Cycle Evolution in the Combustion Chamber of an Oxygen/Kerosene Liquid Rocket Engine
| Authors: Mosolov S.V., Sidlerov D.A. | Published: 22.04.2019 |
| Published in issue: #2(125)/2019 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: liquid rocket engine, combustion chamber, numerical simulation, kerosene combustion | |
Evaluating the Potential of Lithium Hydride in Active Thermal Protection Systems for High-Velocity Aircraft
| Authors: Tovstonog V.A. | Published: 22.04.2019 |
| Published in issue: #2(125)/2019 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
| Keywords: high-velocity aircraft, active thermal protection, phase-change materials, lithium hydride, linear pyrolysis | |
Mathematical Simulation of Using a Combination of Mesh and Porous Materials as a Phase Separator
| Authors: Avraamov N.I., Korolkov A.V., Maslov V.A., Sapozhnikov V.B. | Published: 19.07.2019 |
| Published in issue: #3(126)/2019 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
| Keywords: mathematical simulation, combination of mesh and porous materials, bulk capillary properties, phase separator, in-tank inlet devices, critical retention capacity, residual propellant | |
On the question of computing convective heat transfer parameters in a laminar-to-turbulent boundary layer on an impermeable hemispherical surface
| Authors: Gorskiy V.V., Leonov A.G., Loktionova A.G. | Published: 20.07.2019 |
| Published in issue: #3(126)/2019 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
| Keywords: convective heat transfer, boundary layer, turbulence, viscosity | |
Estimating the Thermal State of a Blunted Wedge in a High-Velocity Gas Flow
| Authors: Zinin K.М., Aliev Az.A., Tovstonog V.A. | Published: 20.07.2019 |
| Published in issue: #3(126)/2019 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
| Keywords: high-velocity aircraft, aero-dynamic heating, thermal protection, refractory oxide materials, thermal state | |
Thermodynamic Design of a Small-Scale Gas Turbine Engine Family
| Authors: Tkachenko A.Yu., Rybakov V.N., Filinov E.P., Ostapyuk Ya.A. | Published: 21.07.2019 |
| Published in issue: #3(126)/2019 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: small-scale gas turbine engine, gas turbine plant, engine family, standardized gas generator, conceptual design, work cycle parameters, non-linear multiple criteria optimization | |
Technique Employing Topology Optimisation to Determine Panel-to-Panel Support Bracket Positions in a Spacecraft Body
| Authors: Borovikov A.A., Leonov A.G., Tushev O.N. | Published: 03.09.2019 |
| Published in issue: #4(127)/2019 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
| Keywords: topology optimisation, finite element method, dynamic compatibility, spacecraft, technique | |