Hey guys,
A new member here. I am looking for some help with Design Data for Constellation 1049. I am in process of creating a 1:1 scaled cad model of the plane`s wing. However, I am unable to determine the chord length for root & tip aifoils from the drawing that I have. I was hoping someone here would be able to help with the process of calculating these chord lengths. Any help will be appreciated. I have attached my reference drawing below.
