Experimental study of damping properties of a composite torsion bar in the helicopter main rotor hingeless hub O. O. DunaiYu. A. DenisovI. N. Sidorov Structural Mechanics and Strength of Flight Vehicles 24 October 2009 Pages: 259 - 263
Finite element analysis of elastic-hysteretic systems with regard to damping A. M. UlanovYu. K. Ponomarev Structural Mechanics and Strength of Flight Vehicles 24 October 2009 Pages: 264 - 270
A refined model of deformation mechanics for laminated composite rods V. A. FirsovI. Sh. GyunalI. S. Selin Structural Mechanics and Strength of Flight Vehicles 24 October 2009 Pages: 271 - 276
Spiral descent of an unmanned aerial vehicle A. V. GomzinE. V. FesenkoV. G. Shataev Flight Dynamics and Control of Flight Vehicles 24 October 2009 Pages: 277 - 283
Methods for constructing diversities of sliding and control of an observation satellite equipped with inertial drives under uncertainty A. S. Meshchanov Flight Dynamics and Control of Flight Vehicles 24 October 2009 Pages: 284 - 295
Investigation of helicopter maneuverability by the power balance method S. A. MikhailovA. Yu. OnushkinS. I. Kochish Flight Dynamics and Control of Flight Vehicles 24 October 2009 Pages: 296 - 301
Maximization of the lift coefficient of airfoils equipped with active flow control devices R. A. Gaifutdinov Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 24 October 2009 Pages: 302 - 309
A model of unsteady swirl flow for calculation of gas exchange in piston internal combustion engines R. D. EnikeevA. A. Chernousov Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 24 October 2009 Pages: 310 - 314
Static strength analysis of aircraft GTE turbine blades and comparison of different calculation methods N. P. VelikanovaA. S. Kiselev Aircraft and Rocket Engine Design and Development 24 October 2009 Pages: 315 - 318
Calculation of axial gasodynamic forces, disk friction losses and overflow in semiopen impellers of centrifugal compressors S. S. Evgen’evG. G. PetrosyanV. A. Futin Aircraft and Rocket Engine Design and Development 24 October 2009 Pages: 319 - 326
Evaluation of the influence of a measurable parameter error on precision of determining αΣ and T g * by regression models N. S. Mel’nikovaD. A. Ionov Aircraft and Rocket Engine Design and Development 24 October 2009 Pages: 327 - 334
On application of the theory of face seals with microgrooves to high-speed FV engine rotors A. I. BelousovS. V. FalaleevA. S. Demura Aircraft and Rocket Engine Theory 24 October 2009 Pages: 335 - 339
Thermal conductivity of thermal barrier coatings A. V. Il’inkovT. A. Il’inkovaR. R. Valiev Aircraft and Rocket Engine Theory 24 October 2009 Pages: 340 - 346
Some possible techniques for improving the strength characteristics of folded cores from sheet composite materials I. M. ZakirovK. A. AlekseevI. R. Gainutdinov Aircraft Production Technology 24 October 2009 Pages: 347 - 350
A method for automation of a process of aircraft hydraulic system modeling M. A. Kovalev Automation of Design and Production of Aeronautical Equipment 24 October 2009 Pages: 351 - 356
Efficiency of a launching booster multinozzle configuration for rockets with out-of-round asymmetrical nozzles A. O. Kochetkov Technical Notes 24 October 2009 Pages: 357 - 360
Arrangement of low-emission combustion in the annular GTE combustion chamber A. N. MarkushinV. K. MerkushinA. V. Baklanov Technical Notes 24 October 2009 Pages: 361 - 364
Influence of input momentum and losses in the turbine on the efficiency of a turbofan engine with periodic fuel combustion V. I. BogdanovA. K. Dormidontov Technical Notes 24 October 2009 Pages: 365 - 367
Calculation of the thermostressed state of a turbine nozzle vane V. A. TrushinR. A. SunarchinV. A. Zinov Technical Notes 24 October 2009 Pages: 368 - 371
Optimization of efficient order service by information unmanned aerial vehicles V. S. MoiseevD. S. GushchinaG. E. Borzov Technical Notes 24 October 2009 Pages: 372 - 375
