Development of the Model 727 Airplane High Lift System

650937

2/1/1965

Authors
Abstract
Content
The development of the model 727 airplane high lift system is treated in two parts: aerodynamics, and structural and mechanical design. Part one explains the high lift requirements and traces flap design evolution from a theoretical viewpoint. It discusses trailing edge flaps, leading edge devices, flap geometry, and transition flaps, and presents results of the flight test program. Part two describes design evolution from a mechanical viewpoint. Flap system configuration and construction are detailed.
Meta TagsDetails
DOI
https://doi.org/10.4271/650937
Citation
Harvey, S. and Norton, D., "Development of the Model 727 Airplane High Lift System," 1965 International Automotive Engineering Congress and Exposition, Detroit, Michigan, United States, January 11, 1965, https://doi.org/10.4271/650937.
Additional Details
Publisher
Published
2/1/1965
Product Code
650937
Content Type
Technical Paper
Language
English