External Blowing Flap Technology on the USAF McDonnell Douglas YC-15

730915

02/01/1973

Event
National Aerospace Engineering and Manufacturing Meeting
Authors Abstract
Content
The YC-15 will be the first aircraft to employ the externally blown flap (EBF)-powered lift system. Since the success of the aircraft to a large extent is dependent on the proper functioning of this system, considerable effort is going into its design. The present paper discusses some of the fundamental aerodynamic considerations which led to the selection of the specific flap configuration and presents resulting aerodynamic characteristics. Structural design criteria for the system and methods of analysis are covered, as are details of the flap-actuating system and structure.
Meta TagsDetails
DOI
https://doi.org/10.4271/730915
Pages
12
Citation
Heald, E., "External Blowing Flap Technology on the USAF McDonnell Douglas YC-15," SAE Technical Paper 730915, 1973, https://doi.org/10.4271/730915.
Additional Details
Publisher
Published
Feb 1, 1973
Product Code
730915
Content Type
Technical Paper
Language
English