Strength analysis of sandwich structures with truss core V. G. Gainutdinov Structural Mechanics and Strength of Flight Vehicles 25 June 2015 Pages: 1 - 6
Analysis of stresses in branched shells of revolution with joint zones using triangular finite elements with allowance for elastoplastic deformation A. Sh. DzhabrailovYu. V. KlochkovS. D. Fomin Structural Mechanics and Strength of Flight Vehicles 25 June 2015 Pages: 7 - 14
Flight path optimization for an electronic intelligence unmanned aerial vehicle K. V. AndreevS. N. Khoroshen’kikhG. V. Moiseev Flight Dynamics and Control of Flight Vehicles 25 June 2015 Pages: 15 - 20
A numerical model for the dynamics of one-velocity gas-vapor-droplet fluid R. I. BayanovA. L. Tukmakov Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 25 June 2015 Pages: 21 - 29
A hybrid model of hypersonic flow Yu. A. RyzhovYu. A. NikitchenkoS. A. Popov Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 25 June 2015 Pages: 30 - 36
Free axisymmetric oscillations of a two-layer liquid with an elastic separator between layers A. A. PozhalostinD. A. Goncharov Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 25 June 2015 Pages: 37 - 41
Advanced designs of elastic damper supports for aircraft engine rotors V. B. Balyakin Aircraft and Rocket Engine Design and Development 25 June 2015 Pages: 42 - 47
Application of neural network approximation methods in the generalization and presentation of the aircraft gas turbine engine turbomachinery characteristics V. A. Grigor’evD. S. KalabukhovV. M. Rad’ko Aircraft and Rocket Engine Theory 25 June 2015 Pages: 48 - 53
The influence of increase in vane leading edge diameter on external heat transfer Yu. G. Gorelov Aircraft and Rocket Engine Theory 25 June 2015 Pages: 54 - 61
A technique for the gas dynamic calculation of the cooled multistage turbine performance B. I. MamaevV. K. Ryabov Aircraft and Rocket Engine Theory 25 June 2015 Pages: 62 - 70
Development of requirements for accuracy of inertia compensation in gas temperature control loop of gas turbine engine control systems with a channel selector V. I. PetuninR. R. SibagatullinA. I. Frid Aircraft Instruments and Instrumentation Computer Complexes 25 June 2015 Pages: 71 - 77
Estimating the influence of hydraulic shot blasting on the endurance limit of hollow cylindrical specimens by the initial deformations of a reference specimen V. A. KirpichevV. P. SazanovO. Yu. Semenova Aircraft Production Technology 25 June 2015 Pages: 78 - 80
Material stress strain behaviour and elastomer pressure under constrained bending of sheet edges O. V. LomovskoiV. K. MoiseevA. A. Sharov Aircraft Production Technology 25 June 2015 Pages: 81 - 87
Determination of processing parameters for the folded core with enveloping curvilinear surface A. A. RazdaibedinV. I. Khaliulin Aircraft Production Technology 25 June 2015 Pages: 88 - 95
Wiring of complicated electrical circuits of interblock assembling in automated design of aircraft E. Yu. FedorovV. S. TereshchukA. V. Ferenetz Automation of Design and Production of Aeronautical Equipment 25 June 2015 Pages: 96 - 99
A technique of determining the wing geometry for an aircraft cable-towed by a carrier L. V. Morozov Technical Notes 25 June 2015 Pages: 100 - 105
Stability of a cylindrical shell under axial compression L. U. BakhtievaF. Kh. Tazyukov Structural Mechanics and Strength of Flight Vehicles 25 June 2015 Pages: 106 - 111
Software for planning and processing the test results for low-thrust liquid rocket engines A. I. KolomentsevA. N. Khokhlov Aircraft and Rocket Engine Design and Development 25 June 2015 Pages: 112 - 115
An experimental study of the effect of vacuum ion-plasma coating deposition on the GTE part cylindrical surface accuracy V. V. BudilovV. S. MukhinI. I. Yagafarov Aircraft Production Technology 25 June 2015 Pages: 116 - 119
Influence of operational life on structure and transient mechanical properties of heat resistant nickel superalloys of stationary gas turbines A. A. Bybin Aircraft Production Technology 25 June 2015 Pages: 120 - 123
Calculation of optimal parameters for multilayer structures of variable height for their manufacture by the method of superplastic forming and diffusion bonding A. V. KolesnikovA. K. ShmakovA. A. Cheslavskaya Aircraft Production Technology 25 June 2015 Pages: 124 - 128
Effect of thermoexposition on residual stresses and limiting amplitude for rolled bolts made of 16KhSN steel V. F. PavlovV. P. RadchenkoM. N. Saushkin Aircraft Production Technology 25 June 2015 Pages: 129 - 132
Pressure determination in impregnation of fabrics by a binder polymer M. S. SalinaYu. P. Kataev Aircraft Production Technology 25 June 2015 Pages: 133 - 136