1964-01-01

Cockpit Landing Visibility 640317

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.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 18% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.

Due to current capacity constraints, printed versions of our publications - including standards, technical papers, EDGE Reports, scholarly journal articles, books, and paint chips - may experience shipping delays of up to four to six weeks. We apologize for any inconvenience.
X