Assertion: duct's entrance | /r/CapableOf | compressor inlet
Facets:
Source sentences:
text: Those areas are diffuser 601, the vortex generator here shown as part of a silencer on the silencer inlet; diffusing duct 602, the vortex generator here shown as a part of the compressor mounted on two stages of blades; diffusing duct 603, the vortex generator here shown mounted on two stages of stators; compressor outlet 604, the vortex generator here shown mounted on a blade row; duct bend 604.5, the vortex generator here shown directing annular segments of flow to follow the contour of the duct; compressor outlet 605, the vortex generator here shown mounted on a stator row; entrance to compressor inlet 606, the vortex generator here shown mounted in an annular flow duct; compressor inlet 607, the vortex generator here shown mounted on a blade row; compressor inlet 608, the vortex generator shown mounted on a stator row; compressor 609, the vortex generator here shown mounted on a stator row; compressor 610, the vortex generator here shown mounted on a blade row; compressor outlet 611, the vortex generator here shown mounted on a blade row; compressor outlet 612, the vortex generator here shown mounted on a turning vane or stator row; diffuser 613, the vortex generator here at the entrance to the combustor; turbine 614, the vortex generator here shown mounted on a blade row upstream of a diffuser; turbine 615, the vortex generator here shown mounted on a stator row upstream of a diffuser; exhaust diffuser 616, the vortex generator here shown mounted between struts; more or less annular diffuser 617, the vortex generator here shown guiding flow along the cone of the tapered center body; duct bend 618, the vortex generator here shown as extensions of turning vanes; and, duct bend 619, the vortex generator here shown that the leading edge in front portion of the turning vane.