High performance airfoil using co-flow jet flow control

43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

Volumn , Issue , 2005, Pages 4813-4839

  Zha, Ge Cheng ^a,c   Carroll, Bruce F ^b   Paxton, Craig D ^a   Conley, Clark A ^a   Wells, Adam ^b  

^a University of Miami College of Engineering   (United States)

^b UNIVERSITY OF FLORIDA   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DRAG; FLOW CONTROL; JETS; KINETIC ENERGY; WIND TUNNELS;

CO-FLOW JETS (CFJ); HIGH PERFORMANCE AIRFOILS; INJECTION SLOT SIZE; JET FLOW CONTROL;

AIRFOILS;

EID: 30744469125     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-1260     Document Type: Conference Paper

References (30)

1. W. L. I. Sellers, B. A. Singer, and L. D. Leavitt, "Aerodynamics for Revolutionary Air Vehicles." AIAA 2004-3785, June 2003.
2. M. Gad-el Hak, "Flow Control: The Future ," Journal of Aircraft, vol. 38, pp. 402-418, 2001.
3. M. Gad-el Hak, Flow Control, Passive, Active, and Reactive Flow Management. Cambridge University Press, 2000.
4. S. Anders, W. L. Sellers, and A. Washburn, "Active Flow Control Activities at NASA Langley." AIAA 2004-2623, June 2004.
5. C. P. Tilmann, R. L. Kimmel, G. Addington, and J. H. Myatt, "Flow Control Research and Application at the AFRL's Air Vehicles Directorate." AIAA 2004-2622, June 2004.
6. D. Miller, , and G. Addington, "Aerodynamic Flowfield Control Technologies for Highly Integrated Airframe Propulsion Flowpaths." AIAA 2004-2625, June 2004.
7. V. Kibens and W. W. Bower, "An Overview of Active Flow Control Applications at The Boeing Company." AIAA 2004-2624, June 2004.
8. V. Modi, M. Fernando, and T. Yokomizo, "Drag Reduction of Bluff Bodies Through Moving Surface Boundary Layer Control." AIAA Paper No. 90-0298, 1990.
9. D. Cichy, J. Harris, and J. MacKay, "Flight Tests of a Rotating Cylinder Flap on a North American Rockwell YOV-10A Aircraft." NASA CR-2135, 1972.
10. R. J. Englar, "Circulation Control Pneumatic Aerodynamics: Blown Force and Moment Augmentation and Modifications; Past, Present and Future. " AIAA 2000-2541, June 2000.
11. L. C. Bradley, "An Experimental Investigation of A Sting-Mounted Finite Circulation Control Wing." M.S. Thesis, Air Force Institute of Technology, 1995.
12. N. Wood, L. Robert, and Z. Celik, "Control of Asymmetric Vortical Flows over Delta Wings at High Angle of Attack," Journal of Aircraft, vol. 27, pp. 429-435, 1990.
13. N. Wood and L. Robert, "Control of Vortical Lift on Delta Wings by Tangential Leading-Edge Blowing," Journal of Aircraft, vol. 25, pp. 236-243, 1988.
14. N. Wood and J. Nielsen, "Circulation Control Airfoils-Past, Present, Future." AIAA Paper 85-0204, 1985.
15. R. J. Englar, L. A. Trobaugh, and R. Hemmersly, "STOL Potential of the Circulation Control Wing for High-Performance Aircraft," Journal of Aircraft, vol. 14, pp. 175-181, 1978.
16. R. J. Englar, "Circulation Control for High Lift and Drag Generation on STOL Aircraft," Journal of Aircraft, vol. 12, pp. 457-463, 1975.
17. A. Smith, "High-Lift Aerodynamics," Journal of Aircraft, vol. 12, pp. 501-530, 1975.
18. J. Lin, S. Robinson, R. McGhee, and W. Valarezo, "Separation Control on High Reynolds Number Multi-Element Airfoils." AIAA Paper 92-2636, 1992.
19. I. Wygnanski, "The Variables Affecting The Control Separation by Periodic Excitation." AIAA 2004-2625, June 2004.
20. K. McManus and J. Magill, "Airfoil Performance Enhancement Using Pulsed Jet Separation Control." AIAA Paper 97-1971, 1997.
21. K. McManus and J. Magill, "Separation Control in Incompressible and Compressible Flows Using Pulsed Jets." AIAA Paper 96-1948, 1996.
22. H. Johari and K. McManus, "Visitation of Pulsed Vortex Generator Jets for Active Control of Boundary Layer Separation." AIAA Paper 97-2021, 1997.
23. Y. Liu, L. N. Sankar, R. J. Englar, K. K. Ahuja, and R. Gaeta, "Computational Evaluation of the Steady and Pulsed Jet Effects on the Performance of a Circulation Control Wing Section." AIAA Paper 2004-0056, 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada 5 - 8 Jan 2004.
24. G.-C. Zha and C. Paxton, "A Novel Airfoil Circulation Augment Flow Control Method Using Co-Flow Jet." NASA/ONR 2004 Circulation Control Workshop, 16-17 March 2004. AIAA Paper 2004-2208, June 2004.
25. G.-C. Zha, (team members: David Car, and W. Copenhaver), "Super Diffusion Cascades Using Co-Flow Jet Flow Control." National Research Council Summer Faculty Final Report, Aug. 23, 2002.
26. J. P. Holman, Experimental Methods for Engineers. New York: McGraw-Hill, 7th Ed., 2001.
27. M. J. Zucrow and J. D. Huffman, Gas Dynamics. John Wiley & Sons, New York, 1976.
28. G. Brown and A. Roshko, "On Density Effects and Large Scale Structure in Turbulent Mixing Layers," Journal of Fluid Mechanics, vol. 64, pp. 675-816, 1974.
29. P. Strykowski, A. Krothapalli, and S. Jendoubi, "The Effect of Counterflow on the Development of Compressible Shear Layers," Journal of Fluid Mechanics, vol. 308, pp. 63-69, 1996.
30. R. Englar and R. M. Williams, "Test Techniques for High Lift, Two Dimensional Airfoils with Boundary Layer and Circulation Control for Application to Rotary Wing Aircraft," Canadian Aeronautics and Space Journal, vol. 19, pp. 93-108, 1973.