TRENDS IN MODERN AIRCRAFT STRUCTURAL DESIGN

570214

01/01/1957

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
Although the Electra structure is based on past good practice, its higher performance and use of prop-jet engines have injected certain new situations of interest to structural engineers. Such items include the new CAA gust criteria, loads created by prop-jet engine failure, development of the “No-Hazard” windshield, engine nacelle design loads, wing loads when taxiing with full wing fuel, fail safe and fatigue, the use of large die forgings, and the bleed air duct system used for de-icing.
Meta TagsDetails
DOI
https://doi.org/10.4271/570214
Pages
14
Citation
SPAULDING, E., "TRENDS IN MODERN AIRCRAFT STRUCTURAL DESIGN," SAE Technical Paper 570214, 1957, https://doi.org/10.4271/570214.
Additional Details
Publisher
Published
Jan 1, 1957
Product Code
570214
Content Type
Technical Paper
Language
English