1-20 of 46079
Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Journal Articles
Journal Articles
Image
Meridional view of the fan stage. Geometry is correct for the computational...
Published Online: August 1, 2022
Fig. 1 Meridional view of the fan stage. Geometry is correct for the computational domain and annotated with differences in the experiment. More
Image
Detail schematic view of the front 1% chord of the rotor blade at three spa...
Published Online: August 1, 2022
Fig. 2 Detail schematic view of the front 1% chord of the rotor blade at three spanwise sections showing damaged leading edge (solid lines) compared with baseline (dotted lines) More
Image
Image
Measured rig characteristics, measured stability limit, and predicted rig b...
Published Online: August 1, 2022
Fig. 4 Measured rig characteristics, measured stability limit, and predicted rig blade characteristics with baseline blade More
Image
Measured rig characteristics, measured stability limit, and predicted engin...
Published Online: August 1, 2022
Fig. 5 Measured rig characteristics, measured stability limit, and predicted engine blade characteristics with baseline and damaged blades More
Image
Computed unsteady static pressure traces on the rig rotor casing at 50% axi...
Published Online: August 1, 2022
Fig. 6 Computed unsteady static pressure traces on the rig rotor casing at 50% axial chord upstream of the LE around the moment of stall inception at three speeds. Time is measured from the moment of the nozzle closure leading to rotating stall. More
Image
Contours of static pressure, limiting streamlines, and green isosurface of ...
Published Online: August 1, 2022
Fig. 7 Contours of static pressure, limiting streamlines, and green isosurface of zero axial velocity on rotor suction surface at the last stable operating point from steady CFD More
Image
Contours of static pressure, limiting streamlines, and green isosurface of ...
Published Online: August 1, 2022
Fig. 8 Contours of static pressure, limiting streamlines, and green isosurface of zero axial velocity on rotor suction surface during stall inception. View of upper part of sectors of three blades extracted from full-annulus unsteady simulations. More
Image
Rotor isentropic Mach number distributions at 95% span at 95% speed from st...
Published Online: August 1, 2022
Fig. 9 Rotor isentropic Mach number distributions at 95% span at 95% speed from steady CFD at last stable point More
Image
Overall and detailed views of contours of relative Mach number in the rotor...
Published Online: August 1, 2022
Fig. 10 Overall and detailed views of contours of relative Mach number in the rotor at 95% span at 95% speed from steady CFD at the last stable point More
Image
Rotor tip leakage axial momentum flux distribution at 95% speed from steady...
Published Online: August 1, 2022
Fig. 11 Rotor tip leakage axial momentum flux distribution at 95% speed from steady CFD at last stable point More
Image
Contours of static pressure, limiting streamlines, and green isosurface of ...
Published Online: August 1, 2022
Fig. 12 Contours of static pressure, limiting streamlines, and green isosurface of zero axial velocity on rotor suction surface at near-stall operating point from steady CFD at 95% speed at last stable point More
Image
Computed unsteady static pressure traces on the rotor casing around the mom...
Published Online: August 1, 2022
Fig. 13 Computed unsteady static pressure traces on the rotor casing around the moment of stall inception for baseline and damaged blades at 95% speed. Time is measured from the moment of the nozzle closure leading to stall. More
Image
Rotor isentropic Mach number distributions at 95% span at 85% speed from st...
Published Online: August 1, 2022
Fig. 14 Rotor isentropic Mach number distributions at 95% span at 85% speed from steady CFD at two operating points More
Image
Overall and detailed views of contours of relative Mach number in the rotor...
Published Online: August 1, 2022
Fig. 15 Overall and detailed views of contours of relative Mach number in the rotor at 95% span at 85% speed from steady CFD at two operating points More
Image
Rotor tip leakage axial momentum flux distributions at 85% speed from stead...
Published Online: August 1, 2022
Fig. 16 Rotor tip leakage axial momentum flux distributions at 85% speed from steady CFD at two operating points More
Image
Contours of static pressure, limiting streamlines, and green isosurface of ...
Published Online: August 1, 2022
Fig. 17 Contours of static pressure, limiting streamlines, and green isosurface of zero axial velocity on rotor suction surface at two near-stall operating points from steady CFD at 85% speed at two operating points More
Journal Articles