Investigation of gyroplane takeoff with the use of main rotor collective pitch A. A. KalmykovV. E. Barsuk Flight Vehicle Design 05 February 2012 Pages: 329 - 333
A software package for computer-aided design analysis of thin-walled structures from composite materials T. Yu. GainutdinovaR. R. Mirkhazov Structural Mechanics and Strength of Flight Vehicles 05 February 2012 Pages: 334 - 340
A lower bound estimate of the critical load for helicopter main rotor composite blade according to the limit equilibrium theory. Analysis results A. V. GorelovI. N. Sidorov Structural Mechanics and Strength of Flight Vehicles 05 February 2012 Pages: 341 - 345
Stress concentration in compressor blades at their damage by foreign objects M. Sh. NikhamkinI. V. Semenova Structural Mechanics and Strength of Flight Vehicles 05 February 2012 Pages: 346 - 350
Dynamics investigation of the two-channel automatic system controlling the mirror of aircraft-based surveillance-search system Yu. M. BelyakovA. I. KarpovV. S. Yatsyk Flight Dynamics and Control of Flight Vehicles 05 February 2012 Pages: 351 - 358
On choice of turbulence models and grid parameters for computation of flows in diffuser ducts B. G. MingazovI. S. Davletshin Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 05 February 2012 Pages: 359 - 366
Application of the parameter-averaging method to calculations of gas ejectors with cylindrical mixing chambers V. I. PanchenkoR. R. Bikbulatov Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 05 February 2012 Pages: 367 - 371
Characteristics of turbine cascade with the modified leading edge of a profile B. I. Mamaev Aircraft and Rocket Engine Design and Development 05 February 2012 Pages: 372 - 378
Computational analysis of strength, stability, and durability for gas turbine engine exhaust frame A. A. RyabovV. I. RomanovA. V. Veselov Aircraft and Rocket Engine Design and Development 05 February 2012 Pages: 379 - 386
Peculiarities of heat transfer in the hemispherical recesses streamlined by a pulsating flow A. V. Il’inkovA. V. ShchukinA. V. Kaurov Aircraft and Rocket Engine Theory 05 February 2012 Pages: 387 - 394
Generalization of experimental data on two-phase critical efflux through axisymmetric channels A. A. LopatinYu. F. GortyshovV. I. Osipova Aircraft and Rocket Engine Theory 05 February 2012 Pages: 395 - 401
Numerical simulation of a boiling up fluid flow in the variable cross-section channels A. L. TukmakovV. G. TonkonogS. A. Kusyumov Aircraft and Rocket Engine Theory 05 February 2012 Pages: 402 - 411
Microindentation of plasma zirconia-based thermal barrier coatings E. A. BarsukovaT. A. Il’inkova Aircraft Production Technology 05 February 2012 Pages: 412 - 416
Theoretical investigation of the vortex zone structure between periodic flow rectangular cross-section turbulators placed on the surface I. E. Lobanov Technical Notes Aircraft and Rocket Engine Theory 05 February 2012 Pages: 417 - 420
Optimization of a tool kit for machining by methods of graph theory L. T. MoiseevaD. V. Kurylev Aircraft Production Technology 05 February 2012 Pages: 421 - 425