Pesquisa

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Autores
Modeling the Transformation of Hexactinal Folded Structure
Shabalov A., Khaliulin V., Gimadiev R., Levshonkov N.
Analysis of Gas Dynamics and Combustion in a Small Reverse-Flow Combustion Chamber
Yousef W., Sychenkov V., Davydov N., Aleksandrov Y.
Numerical Simulation of Detachment Dynamics of a Payload from the Parent Aircraft
Bykov L., Pashkov O., Pravidlo M., Tishkov V., Yanyshev D.
Precision tracking algorithms of civil aircraft by radar information
Sychev M.
Analysis of dynamics of a passive line-of-sight stabilization system with four-axis gimbal suspension
Borodin V., Spiridonov I., Faizutdinov R.
Computational Research of the Main Rotor Steep Descent Modes Based on the Nonlinear Blade Vortex Model
Ignatkin Y., Makeev P., Shaidakov V., Shomov A.
Computational Research of the Main Rotor Hover and Vertical Descent States Based on the Nonlinear Blade Vortex Model
Ignatkin Y., Makeev P., Shaidakov V., Shomov A.
Scaling Effects in the Impact Resistance of Flat and Cylindrical Samples from Composite Materials
Karimbaev T., Chernyshov A.
Application of three-dimensional aerodynamics for calculating trim parameters and flight loads in MSC.Nastran
Kvyatkovskaya M., Leont’eva R.
Development and verification of an analytic technique to determine the stiffness parameters of braided tubular parts
Samipur S., Danilov Y.
Methods of Constructing the Neural Network Models of Regulators for Controlling a Dynamic Object with Smooth Monotonous Behavior
Emaletdinova L., Kabirova A.
Influence of Interference Effects of the Rotor on the Launch Dynamics of Gliding Unmanned Aerial Vehicle
Grumondz V., Al’bokrinova A., Noskov S.
Exploring the Detached-Eddy Simulation for Main Rotor Flows
Dehaeze F., Barakos G., Kusyumov A., Kusyumov S., Mikhailov S.
Model of influence of power line elements on power efficiency of mechatronic modules for advanced mobile objects
Makarenko A., Sorokin A.
Fluid film break-up modeling using adaptive mesh refinement models
Sipatov A., Karabasov S., Gomzikov L., Abramchuk T., Semakov G.
Determination of the Folded Core Geometric Characteristics Based on a Flat-Faceted Elementary Module with Translational Symmetry Considering the Material Thickness
Semeshko M., Alekseev K., Zakiro I., Markovtsev V.
Nonlinear Fracture Resistance Parameters for Elements of Aviation Structures under Biaxial Loading
Shlyannikov V., Zakharov A., Tumanov A.
Aerodynamic Design Method of Integrated Aircraft with Submerged Intake Devices and Power Plant Included into Airframe Carrying System
Kornev A., Sereda V., Migalin K.
Displacement simulation for spacecraft structure
Senashov S., Balyakov D.
Experimental study of the aerodynamics of a wing with various configurations of wingtip triangular extension
Popov S., Djahid G., Kuznetsov A.
Graph Modeling of Data for Assembly Process of GTE Units in Conditions of Production Digitalization
Lyutov A., Ryabov Y., Akh’yanillin N., Davletshin L.
Physical Modeling of Electromagnetic Interference in Unmanned Aerial Vehicle under Action of the Electric Transport Contact Network
Nuriev M., Gizatullin R., Gizatullin Z.
A Technique of Holes Axes Definition in Hidden and Hard-to-Get-to Hardware Zones by Means of Laser Coordinate Measuring Systems
Lyudogovskii P., Komkova M.
A combined model of calculating the durability of aircraft engine high speed rolling bearings
Silaev B., Danilenko P.
Disk wing to main rotor conversion mechanics
Pavlov V., Gasilov M.
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