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Experimental Investigation of a 2D Supercritical Circulation-Control Airfoil Using Particle Image Velocimetry

Author
Allan, Brian G.
Published
[2006].
Physical Description
1 electronic document
Additional Creators
Yao, Chung-Sheng and Jones, Gregory S.
Online Version

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Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Recent efforts in extreme short takeoff and landing aircraft configurations have renewed the interest in circulation control wing design and optimization. The key to accurately designing and optimizing these configurations rests in the modeling of the complex physics of these flows. This paper will highlight the physics of the stagnation and separation regions on two typical circulation control airfoil sections.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 20060022521.
AIAA Paper 2006-3009.
3rd AIAA Flow Control Conference; 5-8 Jun. 2006; San Francisco, CA; United States.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15961753