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Advances in Pneumatic-Controlled High-Lift Systems Through Pulsed BlowingCirculation Control technologies have been around for 65 years, and have been successfully demonstrated in laboratories and flight vehicles alike. Yet there are few production aircraft flying today that implement these advances. Circulation Control techniques may have been overlooked due to perceived unfavorable trade offs of mass flow, pitching moment, cruise drag, noise, etc. Improvements in certain aspects of Circulation Control technology are the focus of this paper. This report will describe airfoil and blown high lift concepts that also address cruise drag reduction and reductions in mass flow through the use of pulsed pneumatic blowing on a Coanda surface. Pulsed concepts demonstrate significant reductions in mass flow requirements for Circulation Control, as well as cruise drag concepts that equal or exceed conventional airfoil systems.
Document ID
20030062153
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Jones, Gregory S.
(NASA Langley Research Center Hampton, VA, United States)
Englar, Robet J.
(Georgia Tech Research Inst. Atlanta, GA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 2003-3411
Report Number: AIAA Paper 2003-3411
Meeting Information
Meeting: 21st Applied Aerodynamics Conference
Location: Orlando, FL
Country: United States
Start Date: June 23, 2003
End Date: June 26, 2003
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available