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Calculation of Aerodynamic Forces on a Propeller in Pitch or Yaw
Report presenting an analysis to determine the applicability of existing propeller theory and the theory of oscillating airfoils to the problem of determining the magnitude of the forces on propellers in pitch or yaw. The steady-state method for calculating propeller forces appears to give satisfactory results.
Date:
February 15, 1949
Creator:
Crigler, John L. & Gilman, Jean, Jr.
System:
The UNT Digital Library