Analysis of static loading of a helicopter tubular skid landing gear S. A. MikhailovL. V. KorotkovD. V. Nedel’ko Structural Mechanics and Strength of Flight Vehicles 08 March 2011 Pages: 369 - 374
Disturbance ranging in capsule atmosphere descent Yu. M. ZabolotnovI. A. Nikonova Flight Dynamics and Control of Flight Vehicles 08 March 2011 Pages: 375 - 381
Modes of Sliding, switching and linear vector control with a given quality of transient processes under uncertainty A. S. Meshchanov Flight Dynamics and Control of Flight Vehicles 08 March 2011 Pages: 382 - 393
Special features of applying the maximal discharge principle and equation of momentum to calculate the flow coefficient for liquid centrifugal atomizers V. I. Zhdanov Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 08 March 2011 Pages: 394 - 400
Modeling of cooling processes in the variable section channel of a gas conduit A.V. KozlovaV. Ya. ModorskiiA. N. Ponik Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 08 March 2011 Pages: 401 - 407
Investigation of gas dynamics numerical schemes based on the solution of one-dimensional test problems N. O. ChukhlantsevaM. V. UsaninA. M. Sipatov Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 08 March 2011 Pages: 408 - 415
An approximated method of calculating the cellular insert influence in the carrying capacity of the direct-flow labyrinth seal E. N. BogomolovS. M. PiotukhV. A. Uglov Aircraft and Rocket Engine Design and Development 08 March 2011 Pages: 416 - 420
Profiling of flow passage in axial radial-flow compressor impellers A. F. KuftovA. V. Syrokvasho Aircraft and Rocket Engine Design and Development 08 March 2011 Pages: 421 - 426
Experimental and theoretical investigation of laser rocket engine characteristics based on a continuous optical discharge A. F. DregalinA. S. CherenkovS. N. Pislegin Aircraft and Rocket Engine Design and Development 08 March 2011 Pages: 427 - 435
Improvement of rich-lean combustion chamber emission at the design stage A. A. InozemtsevV. G. AvgustinovichV. V. Tsatiashvili Aircraft and Rocket Engine Theory 08 March 2011 Pages: 436 - 442
Thermodynamic cycles for spacecraft power plants N. N. Inozemtsev Aircraft and Rocket Engine Theory 08 March 2011 Pages: 443 - 449
A parametric synthesis technique for a stationary multichannel flow-type aerometric receiver in the helicopter air data system A. A. PorunovV. V. Soldatkin Aircraft Instruments and Instrumentation Computer Complexes 08 March 2011 Pages: 450 - 456
Methodology of construction and models of informative signals for a stationary miltichannel flow aerometric receiver of the helicopter air data system A. A. PorunovV. V. SoldatkinV. M. Soldatkin Aircraft Instruments and Instrumentation Computer Complexes 08 March 2011 Pages: 457 - 465
Nonlinear deformation and stability of supported oval cylindrical shells under torsion and bending with internal pressure L. P. ZheleznovV. V. KabanovD. V. Boiko Technical Notes Structural Mechanics and Strength of Flight Vehicles 08 March 2011 Pages: 466 - 469
Investigation of the influence of preliminary buckling for a reinforced medium-filled cylindrical shell on critical stresses of overall instability R. A. IskenderovR. A. Amirova Structural Mechanics and Strength of Flight Vehicles 08 March 2011 Pages: 470 - 474
Development of a high pressure-differential turbine blade cooling system Guanghua Zheng Aircraft and Rocket Engine Design and Development 08 March 2011 Pages: 475 - 478
A two-phase mixture drift flow in the vertical cylindrical channel N. I. KlyuevE. A. Solov’eva Aircraft and Rocket Engine Theory 08 March 2011 Pages: 479 - 482
A two-level system of modeling air-breathing engine afterburners N. S. SenyushkinV. F. Kharitonov Aircraft and Rocket Engine Theory 08 March 2011 Pages: 483 - 486
