1. Simulation of aircraft outlines by means of virtual elastic bodies

   • S. A. Odinokov

   Flight Vehicle Design 13 March 2014 Pages: 319 - 326

2. Analysis of geometrically nonlinear shells of revolution based on the finite element method with the vector interpolation of desired quantities

   • Yu. V. Klochkov
   • A. P. Nikolaev
   • S. S. Marchenko

   Structural Mechanics and Strength of Flight Vehicles 13 March 2014 Pages: 327 - 334

3. Analytical synthesis of functional observers

   • A. Z. Asanov
   • D. N. Dem’yanov

   Flight Dynamics and Control of Flight Vehicles 13 March 2014 Pages: 335 - 343

4. Choice of working parameters of a solid-fuel jet engine of unguided aircraft

   • V. I. Makeev
   • Yu. I. Pushkarev

   Flight Dynamics and Control of Flight Vehicles 13 March 2014 Pages: 344 - 353

5. Effect of local wall heating on the position of the laminar-turbulent transition zone on a blunted cone

   • A. N. Pokrovskii
   • V. N. Shmanenkov

   Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 13 March 2014 Pages: 354 - 358

6. Gas turbine engine disk risk assessment at the design stage taking into account random failures

   • A. I. Belousov
   • A. V. Gritsin

   Aircraft and Rocket Engine Design and Development 13 March 2014 Pages: 359 - 364

7. Experimental studies of lubricant flow processes in radial lemon bore plain bearings

   • L. V. Goryunov
   • V. V. Takmovtsev
   • D. V. Ryabinin

   Aircraft and Rocket Engine Design and Development 13 March 2014 Pages: 365 - 371

8. Thermostressed state in turbine rotor blades with thermal barrier coating at transient conditions of air breathing jet engine operation

   • V. A. Trushin

   Aircraft and Rocket Engine Theory 13 March 2014 Pages: 372 - 378

9. Methods of heat transfer intensification in the thermal stratification pipe

   • A. A. Tsynaeva
   • E. A. Tsynaeva
   • E. V. Shkolin

   Aircraft and Rocket Engine Theory 13 March 2014 Pages: 379 - 383

10. Heat transfer enhancement in combined cooling of the turbine blade leading edge

    • A. V. Shchukin
    • A. V. Il’inkov
    • S. N. Ivanov

    Aircraft and Rocket Engine Theory 13 March 2014 Pages: 384 - 389

11. On influence of tooling geometry and setup parameters on the clinch connection characteristics

    • I. M. Zakirov
    • A. V. Sosov
    • A. V. Nikitin

    Aircraft Production Technology 13 March 2014 Pages: 390 - 395

12. Analysis of light aircraft production management

    • I. Sh. Sharafeev
    • I. V. Ermolenko

    Automation of Design and Production of Aeronautical Equipment 13 March 2014 Pages: 396 - 400

13. Improvement of aircraft GTE emission characteristics by using the microflame fuel combustion in a shortened combustion chamber

    • A. N. Markushin
    • A. V. Baklanov
    • N. E. Tsyganov

    Technical Notes 13 March 2014 Pages: 401 - 406

14. On choice of a swirler for the impulse combustion chamber

    • A. I. Isaev
    • A. M. Safarbakov
    • Yu. I. Mairovich

    Technical Notes 13 March 2014 Pages: 407 - 413

15. A technique for calculating characteristics of axial flow compressor stage with blades of large relative length

    • Yu. A. Rzhavin
    • V. N. Karasev

    Technical Notes 13 March 2014 Pages: 414 - 417

16. Aircraft system for measuring the angular deflections of control surfaces

    • N. D. Koshevoi
    • E. M. Kostenko
    • M. V. Tsekhovskoi

    Aircraft Instruments and Instrumentation Computer Complexes 13 March 2014 Pages: 418 - 422

17. High-strength adhesive joints in aircraft parts

    • V. M. Popov

    Aircraft Production Technology 13 March 2014 Pages: 423 - 430