A technique for calculating large deflections of nonshallow elastoplastic shells of revolution under nonaxisymmetric loading M. S. GaneevaV. E. Moiseeva Structural Mechanics and Strength of Flight Vehicles Pages: 349 - 356
Determination of load-carrying capacity in panels with chevron-type cores R. A. KayumovI. M. ZakirovR. A. Zinnurov Structural Mechanics and Strength of Flight Vehicles Pages: 357 - 361
Influence of climatic operational conditions of a helicopter on physico-mechanical properties of composite materials S. A. MikhailovA. M. GirfanovA. S. Fal’ko Structural Mechanics and Strength of Flight Vehicles Pages: 362 - 367
Dynamic reactions in empennage attachment fittings at control surface deflection M. K. TleulinovA. I. ShigapovV. V. Pavlov Structural Mechanics and Strength of Flight Vehicles Pages: 368 - 373
Diffusion coefficients of multicomponent combustion product mixture O. B. Barysheva Aero-and Gas-Dynamics of Flight Vehicles and Their Engines Pages: 374 - 379
Physical model of a hydrodynamically nonstationary turbulent flow V. M. Kraev Aero-and Gas-Dynamics of Flight Vehicles and Their Engines Pages: 380 - 384
Gasodynamic igniter with an annular nozzle V. V. SemenovI. E. IvanovA. S. Rochev Aero-and Gas-Dynamics of Flight Vehicles and Their Engines Pages: 385 - 389
Problems of application of face gasodynamic seals in aircraft engines A. I. BelousovS. V. FalaleevP. V. Bondarchuk Aircraft and Rocket Engine Design and Development Pages: 390 - 394
Calculation of fuel distribution in the combustion chamber front device equipped with a three-stage swirler V. V. Tret’yakov Aircraft and Rocket Engine Design and Development Pages: 395 - 401
Study of working process instability in the two-chamber solid-propellant rocket engine M. Yu. EgorovYa. V. EgorovS. M. Egorov Aircraft and Rocket Engine Theory Pages: 402 - 408
Noise immunity of automatic GTE control systems with a selector at channel switching modes V. I. PetuninA. I. Frid Aircraft and Rocket Engine Theory Pages: 409 - 414
Theoretical fundamentals for constructing an integrated safety system of airborne ergatic complex operation N. N. Makarov Aircraft Instruments and Instrumentation Computer Complexes Pages: 415 - 421
A system for measuring the altitude-airspeed parameters of rotorcraft and very light flight vehicles M. M. TyurinaA. A. Porunov Aircraft Instruments and Instrumentation Computer Complexes Pages: 422 - 429
To development of air heat pumps for operating in Russian climate B. Kh. Perel’shteinR. A. Kil’deevE. A. Titova Aircraft Instruments and Instrumentation Computer Complexes Pages: 430 - 435
Algorithm for calculating geometry of lifting maximum rigidity surfaces V. G. Gainutdinov Technical Notes Pages: 436 - 438
Residual stresses and endurance strength under tension-compression in the conditions of stress concentration V. F. PavlovV. A. KirpichevD. V. Ivanov Technical Notes Pages: 442 - 445
Influence of propellant components flowrate on the emission characteristics of diffusion flames of coaxial jets S. M. ReshetnikovA. S. Bobrov Aircraft and Rocket Engine Theory Pages: 446 - 449
Thermodynamic properties of gases at combustion of heavy distillate fuels A. B. Shigapov Aircraft and Rocket Engine Theory Pages: 450 - 454
On improvement of strength characteristics in composite polymeric materials by epoxy binders ultrasonic treatment M. M. Ganiev Aircraft Production Technology Pages: 455 - 458
On improvement of materials separation accuracy by superimposition of electric fields A. M. Gren’kovaK. M. Gazizullin Aircraft Production Technology Pages: 459 - 461
