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Vol 59, No 2 (2016)

Flight Vehicle Design

Technique of physical modeling of lightning strike effects on aircraft

Gizatullin Z.M., Gizatullin R.M., Nuriev M.G.

Abstract

This paper considers the issue of direct and indirect effects of lightning strikes on aircraft. It is proposed to study electromagnetic fields and interferences that affect aircraft instruments based on the theory of large-scale experiment.

Russian Aeronautics. 2016;59(2):157-160
pages 157-160 views

Disk wing to main rotor conversion mechanics

Pavlov V.V., Gasilov M.S.

Abstract

A mathematical model of spatial motion of the disk wing blades converted to the main rotor is presented. The system linkage parameters are defined.

Russian Aeronautics. 2016;59(2):161-167
pages 161-167 views

Structural Mechanics and Strength of Flight Vehicles

Fuzzy logic rule as a method for making a design decision in rocketry development

Zezin V.G., Reshetnikov M.I.

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.

Russian Aeronautics. 2016;59(2):168-174
pages 168-174 views

Flight Dynamics and Control of Flight Vehicles

Control synthesis for an unmanned helicopter with time-delay under uncertain external disturbances

Garkushenko V.I., Vinogradov S.S., Barakos G.N.

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.

Russian Aeronautics. 2016;59(2):175-182
pages 175-182 views

The aerospace vehicle control characterizing by considerable time delay

Efremov A.V., Tyaglik M.S., Tyaglik A.S., Aleksandrov V.V.

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.

Russian Aeronautics. 2016;59(2):183-189
pages 183-189 views

Aero- and Gas-Dynamics of Flight Vehicles and Their Engines

Collapse of a spheroidal cavitation bubble near a solid wall

Aganin A.A., Il’gamov M.A., Kosolapova L.A., Malakhov V.G.

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.

Russian Aeronautics. 2016;59(2):190-196
pages 190-196 views

Joint effect of input asymmetrical velocity profile and initial turbulence intensity on hydraulics of a separated diffuser of GTE combustion chamber

Gur’yanova M.M., Piralishvili S.A.

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.

Russian Aeronautics. 2016;59(2):197-205
pages 197-205 views

Experimental investigation of lift for a wing-in-ground effect aircraft model

Nazarov D.V., Frolov V.A., Shakhov V.G.

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.

Russian Aeronautics. 2016;59(2):206-210
pages 206-210 views

Wave resistance defect in a planar flow over periodic reliefs

Semenov V.V., Volkov V.A., Kwon M.C., Sidhu J.S.

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.

Russian Aeronautics. 2016;59(2):211-217
pages 211-217 views

Aircraft and Rocket Engine Design and Development

Experimental investigation of local heat transfer for complex-shaped surfaces using thermochromic liquid crystals

Baibuzenko I.N., Sedlov A.A., Ivanov V.L.

Abstract

This study presents the detailed description of an experimental test rig for local heat transfer measurements as well as the calibration technique and the postprocessing and test run data for a ribbed channel with 45 deg inclined ribs.

Russian Aeronautics. 2016;59(2):218-223
pages 218-223 views

An integrated system of operation mode synchronization for the helicopter powerplant engines

Vel’dyaev A.P., Efanov V.N., Zaitseva A.A.

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.

Russian Aeronautics. 2016;59(2):224-231
pages 224-231 views

Fabrication of filters by a multielectrode tool

Smolentsev V.P., Safonov S.V., Sharov Y.V.

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.

Russian Aeronautics. 2016;59(2):232-236
pages 232-236 views

Aircraft and Rocket Engine Theory

Generalized surge line obtaining jointly with speed lines

Krivosheev I.A., Rozhkov K.E., Simonov N.B.

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.

Russian Aeronautics. 2016;59(2):237-242
pages 237-242 views

A simulator of the aircraft air data system

Efremova E.S.

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.

Russian Aeronautics. 2016;59(2):243-248
pages 243-248 views

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

Shaikin A.P., Galiev I.R.

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.

Russian Aeronautics. 2016;59(2):249-253
pages 249-253 views

Aircraft Production Technology

Research of technological capacities of the process of long-length skin forming by combination of roll-bending and peen forming processing

Malashchenko A.Y.

Abstract

As a result of investigation, the reasons of forming the defects of skin aerodynamic surface shape at roll-bending were determined and technological recommendations on their prevention were provided.

Russian Aeronautics. 2016;59(2):254-258
pages 254-258 views

Quantitative assessment of adhesive contact between carbon fiber and epoxy binding

Nelyub V.A.

Abstract

In this paper, the properties of carbon fibers before and after their gaseous oxidation are evaluated using the RAMAN spectroscopy and electron paramagnetic resonance.

Russian Aeronautics. 2016;59(2):259-262
pages 259-262 views

Radial two-stage microturbine for pneumatic actuation

Kuznetsov Y.P., Khimich V.L., Khrunkov S.N., Krainov A.A.

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.

Russian Aeronautics. 2016;59(2):283-286
pages 283-286 views

Study of shaping strategies for blisk vane channels by a cup tool

Kurylev D.V.

Abstract

This paper deals with roughing milling of vane channels for axial blisks by a cup tool. The effect of the shaping strategy on waviness of the surfaces being machined and allowance for subsequent operations is determined.

Russian Aeronautics. 2016;59(2):287-292
pages 287-292 views

Approach to implementing hardware-independent automatic control systems of lathes and lathe-milling CNC machines

Martinov G.M., Nezhmetdinov R.A., Kuliev A.U.

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.

Russian Aeronautics. 2016;59(2):293-296
pages 293-296 views

Automation of Design and Production of Aeronautical Equipment

Structural optimization of the neural network model for the gas turbine engine monitoring

Novikova S.V.

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.

Russian Aeronautics. 2016;59(2):263-270
pages 263-270 views

Radio Engineering and Communications

Seadrome: Increasing the safety of takeoff and landing operations in the seaplane basin

Voloshchenko V.Y.

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.

Russian Aeronautics. 2016;59(2):271-276
pages 271-276 views

Technical Notes Aircraft Production Technology

Study of thin-walled parts shaping process based on flanging and embossing

Dem’yanenko E.G., Popov I.P.

Abstract

This paper presents the results of analyzing the shaping of thin-walled conical parts with the uniform thickness along generatrix.

Russian Aeronautics. 2016;59(2):277-282
pages 277-282 views