Air Force STOL Tactical Aircraft Investigation: Evaluation of Externally Blown Flaps

730914

02/01/1973

Event
National Aerospace Engineering and Manufacturing Meeting
Authors Abstract
Content
A study of externally blown flaps for application to a medium-sized STOL transport has been completed as part of the U.S. Air Force STOL Tactical Aircraft Investigation program.
Partial results of wind tunnel tests, design trade studies, and flight simulation tests are presented to illustrate the status of externally blown flap technology relative to Air Force STOL transport requirements. It was concluded that the basic technology is adequately developed for attainment of the performance goals. Continuing engineering work is indicated in the areas of flight control system synthesis and component reliability.
Meta TagsDetails
DOI
https://doi.org/10.4271/730914
Pages
15
Citation
Roe, M., "Air Force STOL Tactical Aircraft Investigation: Evaluation of Externally Blown Flaps," SAE Technical Paper 730914, 1973, https://doi.org/10.4271/730914.
Additional Details
Publisher
Published
Feb 1, 1973
Product Code
730914
Content Type
Technical Paper
Language
English