Issue |
Section |
Title |
File |
Vol 8, No 3-1 (2009): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Seal designing in a structure of the cooling system in gas turbine engine |
(Rus)
|
Vol 8, No 3-1 (2009): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Research of a seal work as an element of the air engine support |
(Rus)
|
Vol 8, No 3-1 (2009): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
About the thermal protection of the oil cavities for designing gas turbine engines |
(Rus)
|
Vol 10, No 2 (2011) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Research of gasodynamic seal characteristics under transient conditions of aircraft engines and power plants |
(Rus)
|
Vol 10, No 2 (2011) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Designing a seal as an element of air secondary system in aircraft engines |
(Rus)
|
Vol 11, No 3-3 (2012): Special Issue |
CONFERENCE MATERIALS |
Research of radial face contact seal tightness in the support of the aircraft engine compressor at various operational modes |
(Rus)
|
Vol 11, No 3-3 (2012): Special Issue |
CONFERENCE MATERIALS |
Seal designing as element of aircraft engine systems and engine units |
(Rus)
|
Vol 13, No 5-1 (2014): Special Issue |
ISSUE WITHOUT SECTION |
Analysis of the thermal state of aircraft engine supports |
(Rus)
|
Vol 14, No 3-2 (2015): Special Issue |
ISSUE WITHOUT SECTION |
Research of serviceability of pulsed face seals with pumpback structures |
(Rus)
|
Vol 10, No 3-3 (2011): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Aircraft engine design based on unified gas generator |
(Rus)
|