Issue: #2 (149)
Aviation and Rocket-Space Engineering
Algorithm for Computing the Solid Propellant Rocket Engine with Ballistic Charge in the Aerospace Technology Track Testing
| Authors: Astahov S.A., Kataev A.V., Sizov G.A. | |
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts |
|
| Keywords: rocket track, ballistic solid propellant, specific impulse, strength, stiffness, mass limitations | |
Heat Transfer Comparison with the Non-Axisymmetric Flow Around a Blunt Cone using the FloEFD Commercial Computation Package and Engineering Techniques
On the Authors’ Mathematical Model of the Chelomey’s Pendulum
| Authors: Gribkov V.A., Gordin Ya.D. | |
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. | |
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
Method of the Aircraft Lateral Motion Adaptive Stabilization Taking into Account the Roll Channel Influence
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. | |
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. | |
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
Mechanical Engineering and Machine Science
Numerical Simulation of the Deflection Effect of Meniscus Linings with the Constant Curvature and Thickness Profile on Formation of the High-Speed Elements
| Authors: Baburin M.A., Baskakov V.D., Eliseev S.V., Karnaukhov K.A., Tarasov V.A. | |
Category: Mechanical Engineering and Machine Science | Chapter: Machine Science |
|
| Keywords: high-velocity element, projectile-forming charge, meniscus lining, constant curvature and thickness profile, deflection | |
Organizing the Process of the Time Costs Assessment in Manufacturing the Civilian Product Components at the Military-Industrial Complex Enterprises within the Tender Documentation Preparation Stage
Power Engineering
Simulating Temperature State of Structures with the Power Elements using the Example of an Aircraft Fuel Compartment Exposed to Radiation Heating
| Authors: Gvozdev M.S., Lopukhov I.I. | |
Category: Power Engineering | Chapter: Theoretical and Applied Heat Engineering |
|
| Keywords: radiation heaters, aircraft, fuel compartment, reinforcement elements, combined method, thermal tests | |