Analysis of nonlinear deformation and stability of oval cylindrical shells under combined loading by bending and torsion moments D. V. BoikoL. P. ZheleznovV. V. Kabanov Structural Mechanics and Strength of Flight Vehicles Pages: 235 - 242
Coefficients of equilibrium equations in solving a problem of reconstructing deformation curves for slightly conical thin-walled structures V. A. KostinN. L. Valitova Structural Mechanics and Strength of Flight Vehicles Pages: 243 - 247
Structure of a two-phase flow of boiling water at low-head adiabatic efflux through the laval nozzle Yu. F. GortyshovV. G. TonkonogA. G. Kochenkov Aero-and Gas-Dynamics of Flight Vehicles and Their Engines Pages: 248 - 252
Influence of Archimedes’ forces on turbulent jet development V. N. PosokhinD. V. Maklakov Aero-and Gas-Dynamics of Flight Vehicles and Their Engines Pages: 253 - 261
A theoretical model of convective heat exchange in a turbulent flow A. A. Sergienko Aero-and Gas-Dynamics of Flight Vehicles and Their Engines Pages: 262 - 267
Information technology for adjustment of dynamic processes in aircraft gas turbine engines during the acceptance tests D. A. AkhmedzyanovA. E. Kishalov Aircraft and Rocket Engine Design and Development Pages: 268 - 276
Analysis of the vibrating state of parts and assemblies in the high-pressure compressor of an aircraft engine V. N. Pon’kin Aircraft and Rocket Engine Design and Development Pages: 277 - 281
Application of GTE cycle with heat supply at constant volume V. I. BogdanovE. A. Tarasova Aircraft and Rocket Engine Theory Pages: 282 - 286
Heat transfer in annular channels with flow twisting E. A. BoltenkoG. K. Il’inA. B. Yakovlev Aircraft and Rocket Engine Theory Pages: 287 - 291
Studies of separated flow downstream of the obstacle in a channel at resonant modes of pulsating flow I. A. Davletshin Aircraft and Rocket Engine Theory Pages: 292 - 297
Methods for calculating thermophysical properties of gas mixtures A. F. DregalinO. B. BaryshevaA. S. Cherenkov Aircraft and Rocket Engine Theory Pages: 298 - 302
A mathematical model of vibration combustion in a tube with sudden cross-section change O. V. IovlevaV. M. Larionov Aircraft and Rocket Enging Theory Pages: 303 - 308
Numerical analysis of the coefficients of temperature restitution and heat transfer in high-speed flows N. N. Koval’nogovR. V. Fedorov Aircraft and Rocket Engine Theory Pages: 309 - 316
To a problem on formation of an optimal type of aerial targets V. S. MoiseevA. B. SaleevG. V. Moiseev Automation of Design and Production of Aeronautical Equipment Pages: 317 - 321
Fractal assessment of microaccelerations at weak damping of natural oscillation in spacecraft elastic elements. II A. V. Sedel’nikov Technical Notes Flight Dynamics and Control of Flight Vehicles Pages: 322 - 325
Selection of force parameters of intermolecular interaction potential for a number of individual gases at high temperatures I. V. AnisimovaV. N. Ignat’evR. R. Takseitov Aero-and Gas-Dynamics of Flight Vehicles and Their Engines Pages: 326 - 329
Diagnostics of gas turbine engine blades using the forced vibration method A. V. KocherginI. V. IvshinV. A. Gavrilov Aircraft and Rocket Engine Design and Development Pages: 330 - 332
Prediction of cast gas turbine engine blade quality in industrial environment E. P. KruglovA. A. Porsev Aircraft Production Technology Pages: 333 - 334
Calculation of cutterpath errors in machining GTE monoimpeller vane channels with annular cutting tools A. N. LunevL. T. MoiseevaR. S. Ermakov Aircraft Production Technology Pages: 335 - 339
Checking the permanent joint quality using the hologram interferometry method R. Kh. Makaeva Aircraft Production Technology Pages: 340 - 343
A combined approach to scheduling aperiodic problems in real-time systems S. A. Danilova Automation of Design and Production of Aeronautical Equipment Pages: 344 - 348
