Rational placement and required number of information unmanned aerial systems for on-line monitoring of large territories V. S. MoiseevD. S. GushchinaR. R. Shafigullin Aircraft Equipment 30 November 2012 Pages: 223 - 229
Verification of a mathematical model of dynamic loading in the quasistatic statement for a helicopter tubular skid landing gear by the results of drop tests S. A. MikhailovD. V. Nedel’koS. A. Alimov Structural Mechanics and Strength of Flight Vehicles 30 November 2012 Pages: 230 - 232
Theoretical and experimental technique of determining the mechanical characteristics of folded structure core in the form of Z-crimp. Theoretical foundations and core compression in transverse direction V. N. PaimushinI. I. ZakirovYu. A. Karpikov Structural Mechanics and Strength of Flight Vehicles 30 November 2012 Pages: 233 - 244
Synthesis of the correcting control law to improve the helicopter stabilization quality V. I. GarkushenkoM. V. BezbryazovG. N. Barakos Flight Dynamics and Control of Flight Vehicles 30 November 2012 Pages: 245 - 250
Synthesizing the control system of a small gliding unmanned aerial vehicle with high-aspect ratio wing V. T. GrumondzM. A. PolishchukA. S. Krivoguz Flight Dynamics and Control of Flight Vehicles 30 November 2012 Pages: 251 - 258
Study of roll control system sensitivity to reduction of its order by infinitesimal transformation S. A. DerbenevD. M. Osadchaya Flight Dynamics and Control of Flight Vehicles 30 November 2012 Pages: 259 - 262
Simulation of the flow around a stationary circular cylinder taking into account laminar-turbulent transition A. N. KusyumovE. V. RomanovaG. N. Barakos Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 30 November 2012 Pages: 263 - 268
Radial pressure distribution in lateral clearances of the semi-open axiradial impeller of the centrifugal compressor S. S. Evgen’evV. A. FutinA. V. Zubrinkin Aircraft and Rocket Engine Design and Development 30 November 2012 Pages: 269 - 275
Simulation of conjugate heat transfer under conditions of aero-gas-dynamic heating of anisotropic blunt forebodies of hypersonic aircraft S. A. KolesnikE. L. Kuznetsova Aircraft and Rocket Engine Theory 30 November 2012 Pages: 276 - 283
A simple model of heat exchange and friction in the channels with spiral near-wall flow swirlers V. V. OlimpievB. G. Mirzoev Aircraft and Rocket Engine Theory 30 November 2012 Pages: 284 - 290
Some features of a system for warning the helicopter critical flight regimes V. P. DerevyankinO. I. KuznetsovV. M. Soldatkin Aircraft Instruments and Instrumentation Computer Complexes 30 November 2012 Pages: 291 - 297
Analytical dependences for determination of thermal conduction in sandwich panels with folded cores M. Yu. KiaukaI. M. PonomarevI. Sh. Safin Aircraft Production Technology 30 November 2012 Pages: 298 - 304
To an issue of rating the external loads on a helicopter with skid landing gear for landing loading condition S. A. MikhailovD. V. Nedel’ko Technical Notes 30 November 2012 Pages: 305 - 309
To estimation of moving distributed load effect on the dynamic behavior of circular multilayer cylindrical shells K. A. MoiseevR. S. Mashkov Technical Notes 30 November 2012 Pages: 310 - 314
Modeling the motion of an uncompensated gyrostabilized platform in the Rodrigues-Hamilton parameters V. A. PogorelovE. G. ChubK. Yu. Yakovlev Technical Notes 30 November 2012 Pages: 315 - 319
On correction of profiles in the peripheral sections of turbine unshrouded rotor blades B. I. MamaevI. E. Aleksakhin Technical Notes 30 November 2012 Pages: 320 - 325
Optimimal control of CNC machine operating regimes E. M. Korovin Technical Notes 30 November 2012 Pages: 326 - 331
