Calculation of the effect of thrust-axis inclination on propeller disk loading and comparison with flight measurements

A. W. Vogeley
naca-tn-1721
Oct 1948


An analysis based on simple geometry has been made of the effect of thrust-axis inclination on propeller disk loading. Calculations are in excellent agreement with available flight measurements, so that the analysis is indicated to be adequate for predicting the primary effects of inclination.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1948/naca-tn-1721.pdf