Propeller Design: Practical Application of the Blade Element Theory 1
Description:
"This report is the first of a series of four on propeller design and contains a description of the blade elements or modified Drzewiecke theory as used in the Bureau of Aeronautics, U.S. Navy Department. Blade interference corrections are used which were taken from R.& M. NO. 639 of the British Advisory Committee for Aeronautics. The airfoil characteristics used were obtained from tests of model propellers, not from tests of model wings" (p. 1).
Date:
May 1926
Creator:
Weick, Fred E.
Partner:
UNT Libraries Government Documents Department