Velocity field for an airfoil with co-flow jet flow control

Adam Wells, Clark Conley, Bruce F. Carroll, Craig Paxton, GeCheng Zha

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The wind tunnel tests reported in this paper demonstrate the ability of the co-flow jet airfoil to dramatically increase lift, stall margin, and drag reduction. Detailed velocity field measurements are reported for a baseline NACA0025 airfoil and two variants of the baseline which implement the co-flow jet. The first variant has an injection slot size of 0.65% of chord while the second has an injection slot size twice that size.

Original languageEnglish
Title of host publicationCollection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
Pages10123-10131
Number of pages9
Volume14
StatePublished - Dec 1 2006
Event44th AIAA Aerospace Sciences Meeting 2006 - Reno, NV, United States
Duration: Jan 9 2006Jan 12 2006

Other

Other44th AIAA Aerospace Sciences Meeting 2006
CountryUnited States
CityReno, NV
Period1/9/061/12/06

Fingerprint

jet flow
flow control
airfoils
Airfoils
Flow control
velocity distribution
slots
Drag reduction
injection
Wind tunnels
wind tunnel tests
drag reduction
wind tunnel
drag
margins

ASJC Scopus subject areas

  • Space and Planetary Science
  • Aerospace Engineering

Cite this

Wells, A., Conley, C., Carroll, B. F., Paxton, C., & Zha, G. (2006). Velocity field for an airfoil with co-flow jet flow control. In Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting (Vol. 14, pp. 10123-10131)

Velocity field for an airfoil with co-flow jet flow control. / Wells, Adam; Conley, Clark; Carroll, Bruce F.; Paxton, Craig; Zha, GeCheng.

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. Vol. 14 2006. p. 10123-10131.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Wells, A, Conley, C, Carroll, BF, Paxton, C & Zha, G 2006, Velocity field for an airfoil with co-flow jet flow control. in Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. vol. 14, pp. 10123-10131, 44th AIAA Aerospace Sciences Meeting 2006, Reno, NV, United States, 1/9/06.
Wells A, Conley C, Carroll BF, Paxton C, Zha G. Velocity field for an airfoil with co-flow jet flow control. In Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. Vol. 14. 2006. p. 10123-10131
Wells, Adam ; Conley, Clark ; Carroll, Bruce F. ; Paxton, Craig ; Zha, GeCheng. / Velocity field for an airfoil with co-flow jet flow control. Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting. Vol. 14 2006. pp. 10123-10131
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