All Stories

  1. Algorithm of Forming the Appearance of the Flow Path of Turbomachinery of Two-Shaft Aircraft Engine Core
  2. The Features of Design Calculation Stages of Parameters of Flow Path of Cascade Compressor of Twin Shaft Gas Turbine Engine Core on Base of 1D and 2D Dimensional Models of Their Working Process
  3. Finding Recommendations for Selecting Numerical Model Settings for Efficient Simulation of the Working Process of an Axial Turbine Blade with Convective Cooling
  4. CALCULATING THE PARAMETERS OF A GAS TURBINE ENGINE TAKING INTO ACCOUNT THE UNCERTAINTY OF THE INITIAL DATA
  5. NUMERICAL MODEL OF THE AXIAL TURBINE BLADE COOLING PROCESS
  6. Rational Settings of a Numerical Model to Simulate the Working Process of an Axial-Film-Cooled Turbine Blade
  7. Search for Rational Settings of a Numerical Model of for Studying Film Cooling in Axial Turbines
  8. A method for checking the possibility of joint work of the auxiliary power unit and the starter
  9. Optimization Method of the Multistage Axial Compressors Using CFD Simulation
  10. Optimization of the Workflow of Multistage Axial Compressors Using Modern Gas Dynamics Computing Systems
  11. Improving the start-up parameters of a gas turbine engine by adaptation the air turbine starter
  12. Method of coordinating air starter and auxiliary power unit joint operation
  13. Method for Improving Multi-stage Compressor Parameters using the IOSO Optimizer
  14. Workflow Optimization of Multistage Axial Turbine