1. Investigation of gyroplane takeoff with the use of main rotor collective pitch

   • A. A. Kalmykov
   • V. E. Barsuk

   Flight Vehicle Design 05 February 2012 Pages: 329 - 333

2. A software package for computer-aided design analysis of thin-walled structures from composite materials

   • T. Yu. Gainutdinova
   • R. R. Mirkhazov

   Structural Mechanics and Strength of Flight Vehicles 05 February 2012 Pages: 334 - 340

3. A lower bound estimate of the critical load for helicopter main rotor composite blade according to the limit equilibrium theory. Analysis results

   • A. V. Gorelov
   • I. N. Sidorov

   Structural Mechanics and Strength of Flight Vehicles 05 February 2012 Pages: 341 - 345

4. Stress concentration in compressor blades at their damage by foreign objects

   • M. Sh. Nikhamkin
   • I. V. Semenova

   Structural Mechanics and Strength of Flight Vehicles 05 February 2012 Pages: 346 - 350

5. Dynamics investigation of the two-channel automatic system controlling the mirror of aircraft-based surveillance-search system

   • Yu. M. Belyakov
   • A. I. Karpov
   • V. S. Yatsyk

   Flight Dynamics and Control of Flight Vehicles 05 February 2012 Pages: 351 - 358

6. On choice of turbulence models and grid parameters for computation of flows in diffuser ducts

   • B. G. Mingazov
   • I. S. Davletshin

   Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 05 February 2012 Pages: 359 - 366

7. Application of the parameter-averaging method to calculations of gas ejectors with cylindrical mixing chambers

   • V. I. Panchenko
   • R. R. Bikbulatov

   Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 05 February 2012 Pages: 367 - 371

8. 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

9. Computational analysis of strength, stability, and durability for gas turbine engine exhaust frame

   • A. A. Ryabov
   • V. I. Romanov
   • A. V. Veselov

   Aircraft and Rocket Engine Design and Development 05 February 2012 Pages: 379 - 386

10. Peculiarities of heat transfer in the hemispherical recesses streamlined by a pulsating flow

    • A. V. Il’inkov
    • A. V. Shchukin
    • A. V. Kaurov

    Aircraft and Rocket Engine Theory 05 February 2012 Pages: 387 - 394

11. Generalization of experimental data on two-phase critical efflux through axisymmetric channels

    • A. A. Lopatin
    • Yu. F. Gortyshov
    • V. I. Osipova

    Aircraft and Rocket Engine Theory 05 February 2012 Pages: 395 - 401

12. Numerical simulation of a boiling up fluid flow in the variable cross-section channels

    • A. L. Tukmakov
    • V. G. Tonkonog
    • S. A. Kusyumov

    Aircraft and Rocket Engine Theory 05 February 2012 Pages: 402 - 411

13. Microindentation of plasma zirconia-based thermal barrier coatings

    • E. A. Barsukova
    • T. A. Il’inkova

    Aircraft Production Technology 05 February 2012 Pages: 412 - 416

14. 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

15. Optimization of a tool kit for machining by methods of graph theory

    • L. T. Moiseeva
    • D. V. Kurylev

    Aircraft Production Technology 05 February 2012 Pages: 421 - 425