ALL the performances as well as the strength of an aeroplane are reduced by overloading or increase in gross weight. But, apart from the strength considerations, the maximum…
Abstract
ALL the performances as well as the strength of an aeroplane are reduced by overloading or increase in gross weight. But, apart from the strength considerations, the maximum take‐off weight permissible for the aeroplane probably determines the final limit of overloading, because the aeroplane must at least fly off the ground into the air.
Under this heading are published regularly abstracts of all Reports and Memoranda of the Aeronautical Research Committee, Reports and Technical Notes of the U.S. National Advisory…
Abstract
Under this heading are published regularly abstracts of all Reports and Memoranda of the Aeronautical Research Committee, Reports and Technical Notes of the U.S. National Advisory Committee for Aeronautics and publications of other similar research bodies as issued.