The overall and blade-element performance of a low pressure ratio, low tip speed fan stage at design speed is presented for tow off-design rotor blade angle settings. The rotor design tip speed is 243.8 m/sec and weight flow per unit annulus area is 175.8 kg/sec. Design weight flow and pressure ratio are 29.9 kg/sec and 1.151, respectively.
Performance of low-pressure-ratio fan stage at two off-design blade setting angles
01.03.1977
Report
Keine Angabe
Englisch
British Library Conference Proceedings | 2005
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