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," SAE Technical Paper 650937, 1965, https://doi.org/10.4271/650937.
Additional Details
Publisher
Published
2/1/1965
Product Code
650937
Content Type
Technical Paper
Language
English