affiliation not provided to SSRN
Hypersonic, Precooled airbreathing engine, Thermodynamic cycle, Control law, Working characteristics
aeroengine, Blade tip clearance, blade tip timing, None once per revolution
aeroengine, blade tip clearance, blade tip timing, blade-by-blade
Variable geometry turbine, Wide flow range, Endwall gap, Fan-shaped cascade test, Spherical endwall
Aero-engine, Blade tip timing, Rotating blade, Static deformation, Single-probe
precooler, Pressure Loss, heat transfer, Frosting Patterns, Surface Wettability