


Vol 59, No 2 (2016)
- Year: 2016
- Articles: 23
- URL: https://journal-vniispk.ru/1068-7998/issue/view/14210
Flight Vehicle Design






Structural Mechanics and Strength of Flight Vehicles
Fuzzy logic rule as a method for making a design decision in rocketry development
Abstract
The paper provides a method for multi-criteria selection of the optimal structural layout option based on a fuzzy logic inference that allows for uncertainties in engineering and operates with heterogeneous information of the qualitative and quantitative nature for the systems being designed.



Flight Dynamics and Control of Flight Vehicles
Control synthesis for an unmanned helicopter with time-delay under uncertain external disturbances
Abstract
This paper presents the controller synthesis for an unmanned helicopter with minimum initial information about the parameters of its mathematical model with time-delays of measured and control signals. The unknown parameters, wind disturbances, and system nonlinearity are considered as external disturbances that are estimated using a multi-gap observer. The estimates obtained are used in the control law to improve the stability rate for flight regimes.



The aerospace vehicle control characterizing by considerable time delay
Abstract
In this paper, we propose to compensate the time delay in the vehicle response by a display that demonstrates the vector of predictive velocity projected on the surface located on a preliminary defined distance from the operator’s eyes. The effectiveness of the approach is demonstrated for the tasks of lunar rover docking and control.



Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
Collapse of a spheroidal cavitation bubble near a solid wall
Abstract
Dynamics of a gas bubble in a liquid near a solid wall is studied. The influence of the initial spheroidal disturbances of the bubble shape and the distance to the wall on the dynamics of the bubble–liquid system is analyzed. The pressure in the bubble is initially greater than that of the surrounding liquid. An algorithm based on the Euler scheme and the boundary element method is applied in the calculations.



Joint effect of input asymmetrical velocity profile and initial turbulence intensity on hydraulics of a separated diffuser of GTE combustion chamber
Abstract
This paper presents the regularities of effect of the input asymmetry of the velocity profile on the flow structure in a separated diffuser of the GTE annular combustion chamber. These regularities allow predicting the integral value of hydraulic resistance. We experimentally identified a kind of dependence between the hydraulic losses and Reynolds number in the case of asymmetric velocity profile in a prediffuser assessing the growth of pressure losses. Some updated dependencies are proposed that take into account the joint effect of the input parameters of the working fluid on the integral characteristics of its effectiveness.



Experimental investigation of lift for a wing-in-ground effect aircraft model
Abstract
The aim of the investigation is to develop a technique of recalculating the lift as a function of the angle of attack at different reference points of the aircraft model height over the ground surface. A technique for evaluating the lift of the aircraft model close to the ground surface is proposed.



Wave resistance defect in a planar flow over periodic reliefs
Abstract
The dependence of the wave resistance coefficients for planar periodic reliefs on the similarity parameters is investigated. It is proved that the wave resistance coefficients of the infinite reliefs and their finite analogs in the case of the whole wave numbers coincide, whereas in the case of the fractional wave numbers they differ.



Aircraft and Rocket Engine Design and Development



An integrated system of operation mode synchronization for the helicopter powerplant engines
Abstract
We consider the problem of synthesizing the control system of the helicopter power plant that consists of two turboshaft engines with free turbines, which through an overall mechanical transmission rotate the helicopter uniaxial rotors. We discuss the problem of coordinating the dynamic characteristics of the individual control loops, when the modes of operation are changed with the aim of balancing the load of each of the two engines.



Fabrication of filters by a multielectrode tool
Abstract
The paper deals with the technology of fabricating the filters used in aircraft engines. The new methods of electrochemical dimensional processing are presented, which are used for collective processing of openings with various cross-sections in thin-walled filters.



Aircraft and Rocket Engine Theory
Generalized surge line obtaining jointly with speed lines
Abstract
The analysis and processing results for the known GTE compressor characteristics data are presented. An original method of the universal dimensionless representation of these characteristics is proposed. The dependences obtained are shown in the graphical and analytical form and they are compared with the experimental results.



A simulator of the aircraft air data system
Abstract
This paper considers the purpose, principles of construction, algorithms of generating output signals and the functional diagram of a simulator of aircraft air signals that is built based on the vortex sensor of aerodynamic angle and true airspeed.



Aircraft Instruments and Instrumentation Computer Complexes
Relationship of flame propagation speed for methane–hydrogen fuel of the internal combustion engine with parameters of ion current and hydrogen concentration
Abstract
An indirect method of estimating the visible flame propagation speed of the methane–hydrogen–air mixture with account of carbon content in the fuel mixture and the ion current amplitude is proposed by the experimental results. By comparing the calculated and experimental values, it has been shown that an approach using the methane–hydrogen mixture is advisable at the stage of the internal combustion engine design and development.



Aircraft Production Technology






Radial two-stage microturbine for pneumatic actuation
Abstract
An innovative kinematic scheme of pneumatic turbine drive was proposed and the use of two-row centrifugal-centripetal turbine stage was justified. We proved the feasibility of the proposed kinematic scheme of the turbine drive in a variety of aircraft components by an example of the manual pneumatic grinding machine.






Approach to implementing hardware-independent automatic control systems of lathes and lathe-milling CNC machines
Abstract
We propose the solution of a logical task in CNC system using software-implemented programmable logical controller (Soft PLC). The solution proposed allows unifying the control algorithms of auxiliary equipment of machine tools and reducing the product launch time of new equipment.



Automation of Design and Production of Aeronautical Equipment
Structural optimization of the neural network model for the gas turbine engine monitoring
Abstract
The paper presents a technique of the neural network model reduction for the GTE operation mode monitoring during bench tests. The technique is based on the conversion of the neural network training task to the of multi-criteria optimization task.



Radio Engineering and Communications
Seadrome: Increasing the safety of takeoff and landing operations in the seaplane basin
Abstract
This paper presents the method of preparing the water area of a seaplane basin. It is proposed to use the network structure of the bottom transmitter-receiver antenna assemblies, generating ultrasound in an aqueous medium due to the nonlinear acoustic effects, for echolocation with the adjustable angular resolution of submerged objects.



Technical Notes Aircraft Production Technology


