Selection of rational parameters of physically nonlinear aircraft structures

More works in this specialty

1. 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
2. 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
3. Dynamics of aircraft pipelines

   Kulikov, Yury Alexandrovich · 1995 · Doctor of Sciences

   • 05.07.03 Strength and thermal regimes of aircraft
4. 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
5. 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

All works in this specialty