In connection with tests of airplane cooling systems need was felt for information on axial fan design inasmuch as indications are that such fans will be used in airplane cooling systems in immediate future; fan tested comprised single 24-blade rotor having diam of 21 in. and solidity of 1.33; fan was tested for volume, pressure, and efficiency over range of delivery pressure and volumes for wide range of contravane and blade angle settings.
Test of single-stage axial-flow fan
Nat Advisory Committee Aeronautics -- Report
1941
16 pages
Report
Englisch
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