Treffer 1 - 11 von 11 für Suche 'Zubanov, Vasilii', Suchdauer: 0,24s Treffer weiter einschränken
  1. 1
    Method for Determining the Applicability of an Air Turbine for Operation in a Gas Turbine Engine Launch System
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  2. 2
    GT2021-59589 Comprehensive Performance Improvement for a 16-Stage Axial Compressor
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  3. 3
    Reducing the Hydraulic Resistance in the Inlet Device of the Gas Turbine Unit
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  4. 4
    Optimization of a Single-stage Air Starter Turbine
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  5. 5
    OPTIMIZATION OF AN AIR TURBOSTARTER OF A LAUNCH SYSTEM FOR GAS TURBINE ENGINE
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  6. 6
    GT2020-16034 Optimization of an Air Turbo Starter Considering its Joint Work With an Auxiliary Power Unit
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  7. 7
    MULTIDISCIPLINARY OPTIMIZATION OF A HELICOPTER GTE TURBINE
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  8. 8
    The Influence of the Level of the Flow Path Blockage at the Inlet on the Fan Characteristics
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  9. 9
    THE METHOD OF MATCHING THE JOINT WORK OF THE AUXILIARY POWER UNIT AND TURBOSTARTER AND DETERMINING THE START TIME OF THE GAS TURBINE ENGINE
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  10. 10
    GTINDIA2019-2391 Estimation of the Influence of the Inlet Nonuniformity on the Performance of a Fan of Engine
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  11. 11
    IMPROVEMENT OF THE AERODYNAMIC PARAMETERS OF A 16-STAGE AXIAL COMPRESSOR FOR INDUSTRIAL GAS TURBINE POWER UNIT
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