Thermal, electric-rocket engines and power plants of aircraft

1. Numerical and experimental investigation of the flow in the nozzle of a two-phase gas-droplet flow with a high mass concentration of liquid in the gas

   Yakovlev, Aleksey Aleksandrovich · 2004 · Candidate of Sciences

   • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
2. Study of thermoacoustic heating of gas in gas-jet Hartmann generators

   Li Zhong Min · 2004 · Candidate of Sciences

   • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
3. Friction and heat transfer in the boundary layer on a rough surface

   Zhou Weixin · 2004 · Candidate of Sciences

   • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
4. Influence of the design parameters of a vortex pump on its energy characteristics

   Zhdanov, Igor' Leonidovich · 2004 · Candidate of Sciences

   • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
5. Experimental and computational studies of advanced two-phase thermal control systems for spacecraft and their elements

   Khramov, Sergey Mikhailovich · 2003 · Candidate of Sciences

   • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
6. Theoretical fundamentals and experimental studies aimed at creating flow passages of vane pumps ensuring a combination of high efficiency, suction capability, and low vibration levels

   Chumachenko, Boris Nikolaevich · 2002 · Doctor of Sciences

   • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
   • 05.04.13 Hydraulic machines and hydropneumatic units
7. Contact characteristics and leak-tightness of fixed joints of pneumohydraulic fuel systems of aircraft engines

   Ogar, Pyotr Mikhailovich · 1997 · Doctor of Sciences

   • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
8. Improving the operational performance of gas turbine engine blades through adaptive preparation of their manufacturing technology

   Ji, Zhenyu · 1995 · Candidate of Sciences

   • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
9. Development and experimental verification of a calculation method, and analysis of the specific features of the performance characteristics of the counter-rotating turbine of a gas turbine engine without an intermediate nozzle vane ring

   Favorskaya, Natalia Olegovna · 1993 · Candidate of Sciences

   • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
10. Effect of heat exchange processes on the operability of hydrostatic-dynamic bearings of liquid-propellant rocket engine turbopumps

    Koveza, Yuriy Vladimirovich · 1992 · Candidate of Sciences

    • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
11. Method and algorithms for forming the configuration of a turbocompressor of helicopter gas turbine engines in a CAD system

    Sivtsov, Yuriy Mikhaylovich · 1992 · Candidate of Sciences

    • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
    • 05.13.12 Computer-aided design systems (by industry)
12. Development, investigation and implementation of a method for cooling gas turbine engine components with vortex energy separators

    Zhornik, Irina Vladimirovna · 1992 · Candidate of Sciences

    • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft
13. Calculation of technological parameters of non-stationary processes of electrochemical dimensional machining of gas turbine engine parts

    Yastrebov, Valeriy Nikolaevich · 1991 · Candidate of Sciences

    • 05.07.05 Thermal, electric-rocket engines and power plants of aircraft