hi guys
When calculating the shear strength with the schrenk method of a rectangular wing I understand that i should use the chord minus the flap chord. Is that right? Textbooks use the total wing chord but i understand that this is simplification
When calculating the shear strength with the schrenk method of a rectangular wing I understand that i should use the chord minus the flap chord. Is that right? Textbooks use the total wing chord but i understand that this is simplification