Vol 61, No 1 (2018)
- Year: 2018
- Articles: 23
- URL: https://journals.rcsi.science/1068-7998/issue/view/14261
Flight Vehicle Design
Aerodynamic Design Method of Integrated Aircraft with Submerged Intake Devices and Power Plant Included into Airframe Carrying System
Abstract
This paper presents a theoretically and practically grounded architecture of design methods combination. A possibility and completeness of developing integral design solutions and intensifying the design process are provided by redistribution of emphases of numerical and natural experiments.
Aircraft Equipment
Optical Design for a Cubesat: Unobscured Telescope, Using Freeform Mirrors and a Curved Detector
Abstract
The possibility of constructing an optical scheme of a telescope for a small satellite based on mirrors with freeform surfaces and a curved photodetector is considered. It is shown that the use of a new element base allows the effective area of the main mirror to be maximized and the field of view up to 9.4 times to be increased in comparison with the classical scheme of the Ritchey–Chretien scheme in ensuring the high image quality.
Flight Dynamics and Control of Flight Vehicles
Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
Exploring the Detached-Eddy Simulation for Main Rotor Flows
Abstract
This paper applies the Detached-Eddy Simulation (DES) method to resolve a larger part of the flow spectrum around rotor blades in hover and forward flight. A comparison between DES and Unsteady Reynolds–Averaged Navier–Stokes simulation was carried out for the case of a forward flying rotor suggesting that DES has great potential for rotor applications.
Aircraft and Rocket Engine Design and Development
The 3D Computational Investigation of Film Cooling Effectiveness for Turbine Nozzle Vanes with “Meridian Constriction” and Shaped Film-Cooling Holes
Abstract
Active influence dimension of film cooling along the blade profile is investigated with using the Spalart–Allmaras turbulence model. The cooling effectiveness of vane platforms and vane fillets is studied with the use of perforation holes on the leading edge.
Development of the Technique for Calculating the Ejectors with Low Entrainment Ratios
Abstract
This paper presents the results of an investigation of ejectors with the low entrainment ratio. A technique for calculating the ejectors with a curvilinear axis has been developed. Comparative studies of the performance characteristics of ejectors with the rectilinear axis of the mixing chamber and the curvilinear initial section of the mixing chamber are carried out.
Aircraft and Rocket Engine Theory
To Calculation of Regenerative Cooling of a Liquid Fuel Rocket Engine Chamber
Abstract
This paper demonstrates that in transition from the one-dimensional longitudinal-channel motion of the coolant in the regenerative cooling system of the liquid propellant engine to the twodimensional (interchannel) channel motion (transpiration) through a porous mesh material (PMM), the hydraulic losses decrease. Experimental data on PMM hydraulic resistance coefficients and heat transfer in porous paths with the interchannel coolant transpiration (ICCT) is presented.
Use of a Nonlinear Mathematical Model of Turboprop Engine on a Semi-Full-Scale Simulation Test Bench for Testing Propellers in Conjunction with Their Automatic Control System
Abstract
This paper considers an issue of increasing reliability of turboprop engine simulation on a semi-full-scale simulation test bench. A detailed mathematical model (subassembly model) of a turboprop engine is used for improving simulation quality and optimizing the algorithms of turboprop automatic control system in the operation conditions being expected.
Aircraft Production Technology
Determination of Slag Retention Ability of Gating Systems
Abstract
The paper highlights results of analyzing the gating systems in terms of assurance of slag retention at the stage when the mold cavity is filled up with the melt. Quantitative values of parameters as to assessment of slag retention were obtained that can be applied in selecting the gating system type for a casting.
Gas and Powder Flow Optimization in a Four-Jet Laser Cladding Head
Abstract
Gas and powder flow structure in a four-jet nozzle of a laser cladding head was optimized using a shadow imaging device and high-speed tracer visualization. Experimental results show that an excessive protective gas flow rate can lead to the spatial defocusing of transport gas jets.
Radio Engineering and Communication
Seadrome: Technologies of Complex Navigation for Amphibious Unmanned Aerial Vehicles in the Seaplane Basin
Abstract
The paper considers the physical principles of operation, performance and structural diagram of the short base sonar navigation system installed aboard an amphibious unmanned aerial vehicle. This system provides the required course piloting in the seaplane basin that is assigned by the network system of bottom transmitter-receiver antenna assemblies.
Cognitive Graphical Additions to the Interfaces of Command Measurement Systems for Aerospace Application
Abstract
The methods of cognitive graphical information presentation are considered to support decision-making in earth stations of command measurement systems. The work is performed on transforming telemetric data, readings of the sensors of space module and earth station into visual images.
To a Matter of Increasing the Spectral Efficiency of Phase Radio-Technical Data Transmission Systems Operating under Strong Intersymbol Interference
Abstract
This paper analyzes the possibility of increasing the spectral efficiency of phase radio-technical data transmission systems that operate under conditions of mutual interference of symbols when “transparency windows” are used. The conditions for emergency of “transparency windows” are defined, recommendations for their application with the purpose of increasing the spectral efficiency of communication systems being considered are presented. Changes in time characteristics of “transparency windows” are analyzed (their lengths over the range of channel symbol time duration) depending on the frequency detuning.
Technical Notes Structural Mechanics and Strength of Flight Vehicles
Scaling Effects in the Impact Resistance of Flat and Cylindrical Samples from Composite Materials
Abstract
The scaling factors in the problems of assessing the resistance to high-speed impact of plates and shells are analytically determined. Numerical experimentation shows the possibility of applying certain scaling factors in assessing the impact resistance of laminated plates and shells from materials with orthotropic properties.
Structural Mechanics and Strength of Flight Vehicles
Sensitivity Algorithm as a Solution of an Inverse Strength Problem Applied to Thin-Walled Structures
Abstract
The problem of identifying rigidities in stiffeners of a four-stiffener torsion box operating in tension–compression under the action of an external load is considered. An iterative approach is proposed using a sensitivity function and a sensitivity matrix.