Cockpit design of modern highspeed aircraft has become greatly complicated by the need for providing sufficient visual field coverage for the pilot during take-off and landing. This paper is concerned with the problem of specifying minimum required down angles for forward and side vision from the cockpit. A method based on theoretical assumptions is presented, and includes a formula that considers the various factors involved.
Cockpit Landing Visibility
Sae Technical Papers
SAE World Congress & Exhibition ; 1964
01.01.1964
Aufsatz (Konferenz)
Englisch