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Lifting Force Estimation for Aerodesign by Ali is a document available to read on EtoBox.

This document presents a new approach for estimating the distribution of lifting forces along the wingspan of an Aerodesign class airplane using a modified Schrenk approximation method. The method calculates lifting distributions based on the average between elliptical and trapezoidal wing distributions. A new proportionality factor using dimensionless velocity is introduced to estimate load distributions for different maneuvers in the aircraft

Author

Ali

Language

EN