Aerodynamics and Loss Accounting of a Low Pressure Ratio Fan for an Over-Wing Mounted Engine
VALIDATION OF A SYSTEM THEORY MODEL FOR AIRCRAFT ENGINE SIMULATION (AIAA 2017-3830)
Investigation of a Diesel Engine for Aircraft Application (AIAA 2017-4792)
Potential of Static Pressure Recovery of Rotor-Only Low-Pressure Axial Fans
Surface roughness of real operationally used compressor blade and blisk
On the Impact of Condensation and Liquid Water on the Radial Turbine of a Fuel Cell Turbocharger