Strength and thermal regimes of aircraft

1. Method and algorithm for calculating the elastic-mass characteristics of high-aspect-ratio wing models based on the hydrodynamic analogy

   Tran, Van Hung · 2016 · Candidate of Sciences · Zhukovsky Central Aerohydrodynamic Institute

   • 05.07.03 Strength and thermal regimes of aircraft
2. Development of a compartment method for calculating vibrations of composite axisymmetric thin-walled structures with liquid

   Rei, Chzhunbum · 2013 · Candidate of Sciences · Moscow State Aviation Institute

   • 01.02.06 Dynamics and strength of machines, instruments and apparatus
   • 05.07.03 Strength and thermal regimes of aircraft
3. Investigation of the loading and strength of a helicopter main rotor blade under maneuvering and transient conditions

   Averyanov, Igor Olegovich · 2012 · Candidate of Sciences · Russian State Technological University named after K. E. Tsiolkovsky (MATI)

   • 05.07.03 Strength and thermal regimes of aircraft
4. Solution of problems of nonlinear deformation and stability of shells by the finite element method

   Zheleznov, Lev Petrovich · 2009 · Doctor of Sciences · Novosibirsk State Technical University

   • 05.07.03 Strength and thermal regimes of aircraft
5. Calculation of multi-cell anisotropic shells of the wing box type

   Shcherbakov, Iurii Viktorovich · 2002 · Candidate of Sciences

   • 05.07.03 Strength and thermal regimes of aircraft
6. Methods and means of constructing effective measuring information systems for studying the strength of aircraft structures

   Shevchuk, Vyacheslav Vasil'yevich · 2002 · Doctor of Sciences

   • 05.07.03 Strength and thermal regimes of aircraft
7. Development of a calculation method for the stress-strain and limit state of multilayer composite torsion bars of hingeless helicopter rotors

   Shuvalov, Vladimir Aleksandrovich · 2002 · Candidate of Sciences

   • 05.07.03 Strength and thermal regimes of aircraft
   • 01.02.04 Mechanics of deformable solids
8. Applied methods for calculating thermomechanical joints of pipelines of pneumatic-hydraulic systems of aircraft

   Shishkin, Sergey Vilenovich · 1999 · Doctor of Sciences

   • 05.07.03 Strength and thermal regimes of aircraft
   • 05.07.04
9. Investigation of dynamic processes of an elastic aircraft with liquid fuel based on a multilevel computational model

   Tukbaev, Rais Khusnullovich · 1999 · Candidate of Sciences

   • 05.07.03 Strength and thermal regimes of aircraft
10. A theoretical-experimental method for the study of free vibrations of elements of aircraft structures of complex geometry

    Shikhalov, Maksim Lvovich · 1998 · Candidate of Sciences

    • 05.07.03 Strength and thermal regimes of aircraft
11. Selection of rational parameters of physically nonlinear aircraft structures

    Chekhov, Vladimir Valer'yevich · 1998 · Candidate of Sciences

    • 05.07.03 Strength and thermal regimes of aircraft
12. Development of methods and equipment for service life testing of the taxiing damping devices of aircraft landing gear

    Filatov, Valentin Aleksandrovich · 1997 · Candidate of Sciences

    • 05.07.03 Strength and thermal regimes of aircraft
13. Nonlinear interaction of aircraft structures with the soil foundation

    Zharkov, Oleg Aleksandrovich · 1997 · Candidate of Sciences

    • 05.07.03 Strength and thermal regimes of aircraft
14. Dynamics of aircraft pipelines

    Kulikov, Yury Alexandrovich · 1995 · Doctor of Sciences

    • 05.07.03 Strength and thermal regimes of aircraft
15. Methodology for analyzing the elastic dynamic stability of aerospace systems

    Zuyev, Aleksey Arsent'yevich · 1994 · Candidate of Sciences

    • 05.07.03 Strength and thermal regimes of aircraft
16. Strength of the tail sections of a helicopter main rotor blade

    Surovtseva, O. E. · 1994 · Candidate of Sciences

    • 05.07.03 Strength and thermal regimes of aircraft
17. Nonstationary deformation of layered shell elements of aircraft structures of complex geometry preloaded with a static load

    Grozmani, Yuriy Borisovich · 1993 · Candidate of Sciences

    • 05.07.03 Strength and thermal regimes of aircraft
18. Application of the method of interpolation polynomials in calculating the statistical dynamics of aircraft transportation

    Minoransky, Roman Eduardovich · 1993 · Candidate of Sciences

    • 05.07.03 Strength and thermal regimes of aircraft
19. Load-bearing capacity of aircraft structural elements of the sandwich composite shell type with allowance for delamination

    Skvortsov, Yuriy Vasil'yevich · 1992 · Candidate of Sciences

    • 05.07.03 Strength and thermal regimes of aircraft