Journal article
Numerical study of wind-tunnel sidewall effects on circulation control airfoil flows
- Abstract:
-
Two-and three-dimensional numerical simulations are performed of the flow around a circulation control airfoil (using a Coanda jet blowing overarounded trailing edge) placed in a rectangular wind-tunnel test section. The airfoil model spans the entire tunnel and the span-to-chord ratio of the model is 3.26. The objective of this numerical study, in which we solve the compressible Reynolds-averaged Navier-Stokes equations in a time-resolved manner (but the solutions eventually converge to stea...
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- Publisher copy:
- 10.2514/1.J050328
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Authors
Bibliographic Details
- Journal:
- AIAA Journal
- Volume:
- 48
- Issue:
- 9
- Pages:
- 2123-2132
- Publication date:
- 2010-09-01
- DOI:
- EISSN:
-
1533-385X
- ISSN:
-
0001-1452
- Source identifiers:
-
300742
Item Description
- Language:
- English
- Pubs id:
-
pubs:300742
- UUID:
-
uuid:b610a388-453e-4394-aad2-12352b3cddcd
- Local pid:
- pubs:300742
- Deposit date:
- 2012-12-19
Terms of use
- Copyright date:
- 2010
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