Upper Surface Blowing Technology as Applied to the YC-14 Airplane

730916

02/01/1973

Event
National Aerospace Engineering and Manufacturing Meeting
Authors Abstract
Content
The exhaust from a high bypass ratio turbofan engine, passing over the upper surface of a wing and trailing edge flap system, can be deflected by the Coanda effect to create both deflected thrust and supercirculation. This technique, known as “upper surface blowing,” has been applied to the U.S. Air Force/Boeing YC-14 advanced medium STOL transport airplane. Laboratory and wind tunnel tests have shown very efficient turning of the jet flow, large values of supercirculation, and excellent boundary layer control of the external flow on the upper surface of the wing. This combination creates a powered lift system having unusual efficiency and versatility.
Meta TagsDetails
DOI
https://doi.org/10.4271/730916
Pages
8
Citation
Wimpress, J., "Upper Surface Blowing Technology as Applied to the YC-14 Airplane," SAE Technical Paper 730916, 1973, https://doi.org/10.4271/730916.
Additional Details
Publisher
Published
Feb 1, 1973
Product Code
730916
Content Type
Technical Paper
Language
English