Candidate Engines Definition for Future Multi Speed Supersonic Civil Aircraft
Integration of a High-Pressure Gas Turbine of the Gas Turbine Engine with a Gas-Dynamic Laser
Integration of a High-Pressure Gas Turbine of the Gas Turbine Engine with a Gas-Dynamic Laser
Development of a Particle–Particle Hybrid Scheme to Simulate Multiscale Transitional Flows
Development of a Particle-Particle Hybrid Scheme to Simulate Multiscale Transitional Flows
Investigation of power gas turbine drives on the basis of mathematical models
Investigation of power gas turbine drives on the basis of mathematical models