Through application of linearized theory compressibility correction is obtained which gives thrust or torque coefficient in subsonic flow, for propeller or helicopter rotor, directly from incompressible flow values.
Subsonic compressibility corrections for propellers and helicopter rotors
J. Aeronautical Sciences
Journal of the Aeronautical Sciences ; 20 , n 10
1953
8 pages
Article (Journal)
English
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Static thrust analysis for helicopter rotors and airplane propellers
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