PERFORMANCE OF A HIGHLY LOADED TWO-STAGE AXIAL-FLOW FAN

摘要

A two-stage axial-flow fan with a tip speed of 1450 ft/sec (442 m/sec) and an overall pressure ratio of 2.8 was designed, built, and tested. At design speed and pressure ratio, the measured flow matched the design value of 184.2lbm/sec (83.55 kg/sec). The adiabatic efficiency at the design operating point was 85.7 percent. The stall margin at design speed was 10 percent. A first-bending-mode flutter of the second-stage rotor blades was encountered near stall at speeds between 77 and 93 percent of design, and also at high pressure ratios at speeds above 105 per¬cent of design. A 5° closed reset of the first-stage stator eliminated second-stage flutter for all but a narrow speed range near 90 percent of design.