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1
Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0 to 180 degrees /
Published 1954“…Y 3.N 21/5:6/3228…”
Government Document Book -
2
Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0° to 180° /
Published 1954“…Y 3.N 21/5:6/3228…”
Online Access
Government Document eBook