Heat Transfer Comparison with the Non-Axisymmetric Flow Around a Blunt Cone using the FloEFD Commercial Computation Package and Engineering Techniques
Authors: Brodskiy M.Yu. | Published: 08.07.2024 |
Published in issue: #2(149)/2024 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: asymmetric flow-around, heat transfer, equilibrium temperature, boundary layer, effective length method, FloEFD computation complex |
On the Authors’ Mathematical Model of the Chelomey’s Pendulum
Authors: Gribkov V.A., Gordin Ya.D. | Published: 08.07.2024 |
Published in issue: #2(149)/2024 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: inverted pendulum, parametric excitation, stabilization, stability, Chelomey’s pendulum |
Processing of Modal Test Results Taking into Consideration the Damping Nonlinear Dependence on the Oscillation Frequency
Authors: Dmitriev S.N., Khamidullin R.K.  | Published: 08.07.2024 |
Published in issue: #2(149)/2024 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: мodal analysis, oscillation testing, nonlinear damping, oscillation damping, transfer function |
Adaptive Antenna Array Introduction for the Satellite Navigation System Users
Authors: Ermilov A.S., Balashov A.Yu., Gyulmagomedov N.Kh., Evseev D.A. | Published: 08.07.2024 |
Published in issue: #2(149)/2024 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: antenna array design, micro-strip antenna, setup development, additive technologies, satellite navigation user equipment, 3D printing, technical solutions development |
Method of the Aircraft Lateral Motion Adaptive Stabilization Taking into Account the Roll Channel Influence
Authors: Zenchenko M.V., Tochilova O.L. | Published: 08.07.2024 |
Published in issue: #2(149)/2024 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: adaptive stabilization, identification, aerodynamic characteristics, restoration, unmeasured coordinates, state vector, perturbed lateral motion |
Simulating Heat Flows Supplied to the Surface of a Blunt Convex Rotation Body in the Supersonic Gas Flow
Authors: Kotenev V.P., Resh V.G., Sysenko V.A. | Published: 08.07.2024 |
Published in issue: #2(149)/2024 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: heat flow, boundary layer, axisymmetric gas flow, sound point |
Linear Mechanical System Dynamics under the Influence of Additive and Multiplicative Polyharmonic High-Frequency Effects with the Non-Multiple Frequencies
Authors: Tushev O.N., Kondratyev E.K. | Published: 22.07.2024 |
Published in issue: #2(149)/2024 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: linear system, additive influences, parametric influences, slow motion, fast motion, segregation, resonance, constant component |
Comparative Analysis of the Propulsion System Mass for a Small Space Tug
Authors: Shcheglov G.A., Shapovalov A.V. | Published: 24.07.2024 |
Published in issue: #2(149)/2024 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: small space tug, propulsion system, pressure feed system, gaseous propellant components, mass analysis, design parameter analysis |
Computing Thermal Protection of the Soil-Sampling Mechanism Drive of the Venera-D Automatic Interplanetary Station Exposed to Extreme Operation Conditions
Authors: Koveshnikov A.A., Paleshkin A.V. | Published: 18.09.2024 |
Published in issue: #3(150)/2024 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: thermal protection, Venera-D, thermodynamics, thermal insulation, heat accumulator, phase transition, mathematical model |
Numerical Simulation of the NK-38ST Gas Turbine Engine Combustion Chamber CO Emission Depending on the Ambient Temperature
Authors: Tikhonov O.A., Sabirzyanov A.N., Baklanov A.V. | Published: 18.09.2024 |
Published in issue: #3(150)/2024 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
Keywords: gas turbine unit, combustion chamber, mathematical model, numerical simulation, kinetic mechanism, emission |