Computational evaluation of the steady and pulsed jet effects on the performance of a circulation control wing section

AIAA Paper

Volumn , Issue , 2004, Pages 4192-4206

  Liu, Yi ^a   Sankar, Lakshmi N ^a   Englar, Robert J ^a   Ahuja, Krishan K ^a   Gaeta, R ^a  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; AIRCRAFT LANDING; JETS; NAVIER STOKES EQUATIONS; NOISE POLLUTION; STEADY FLOW; TAKEOFF; VORTEX FLOW;

CIRCULATION CONTROL TECHNOLOGY; CIRCULATION CONTROL WING (CCW); PULSED JET EFFECTS;

WINGS;

EID: 2942753911     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-56     Document Type: Conference Paper

References (21)

1. Englar, Robert J., Smith, Marilyn J., Kelley, Sean M. and Rover, Richard C. III., "Application of Circulation Control to Advanced Subsonic Transport Aircraft, Part I: Airfoil Development," Journal of Aircraft, Vol.31 No.5, pp. 1160-1168, Sep. 1994.
2. Englar, Robert J., Smith, Marilyn J., Kelley, Sean M. and Rover, Richard C. III., "Application of Circulation Control to Advanced Subsonic Transport Aircraft, Part II: Transport Application," Journal of Aircraft, Vol.31, No.5, pp. 1169-1177, Sep. 1994.
3. Shrewsbury, G. D. and Sankar, L. N., "Dynamic stall of an oscillating circulation control airfoil," International Symposium on Nonsteady Fluid Dynamics, Toronto, Canada, June 4-7, 1990, Proceedings. New York, American Society of Mechanical Engineers, pp. 15-22, 1990.
4. Shrewsbury, G. D. and Sankar, L. N., "Dynamic Stall of Circulation Control Airfoils," AIAA Paper 90-0573, January 1990.
5. Salikuddin, M., Brown, W. H. and Ahuja, K. K., "Noise From a Circulation Control Wing with Upper Surface Blowing," Journal of Aircraft, Vol.24, pp55-64, Jan. 1987.
6. Englar, R. J. and Huson, G. G., "Development of Advanced Circulation Control Wing High Lift Airfoils," AIAA paper 83-1847, presented at AIAA Applied Aerodynamics Conference, July, 1983.
7. Munro, S., Ahuja, K., and Englar, R., "Noise Reduction Through Circulation Control Technology," AIAA Paper 2001-0666, Jan. 2001.
8. th AIAA/CEAS Aeroacoustics Conference and Exhibit, Hilton Head, South Carolina, 12-14 May 2003.
9. th AIAA/CEAS Aeroacoustics Conference and Exhibit, Hilton Head, South Carolina, 12-14 May 2003.
10. th AIAA/CEAS Aeroacoustics Conference and Exhibit, Hilton Head, South Carolina, 12-14 May 2003.
11. Liu, Y., "Numerical Simulations of the Aerodynamic Characteristics of Circulation Control Wing Sections," Ph.D Thesis, Georgia Institute of Technology, 2003.
12. Liu, Y., Sankar, L. N., Englar, R. J. and Ahuja, K. K., "Numerical Simulations of the Steady and Unsteady Aerodynamic Characteristics of a Circulation Control Wing Airfoil," AIAA paper 2001-0704, January 2001.
13. Kwon, J. and Sankar, L.N., "Numerical Study of the Effects of Icing on Finite Wing Aerodynamics," AIAA Paper 90-0757.
14. Bangalore, A., Phaengsook, N. and Sankar, L. N., "Application of a Third Order Upwind Scheme to Viscous Flow over Clean and Iced Wings," AIAA Paper 94-0485.
15. Baldwin, B. S., and Lomax, H., "Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows," AIAA Paper 78-257, Jan. 1978.
16. Spalart, P. R., and Allmaras, S. R., "A One-Equation Turbulence Model for Aerodynamic Flows," AIAA Paper 92-0439, Jan. 1992.
17. Shrewsbury, G. D., "Numerical Evaluation of Circulation Control Airfoil Performance Using Navier-Stokes Methods," AIAA paper 86-0286, January 1986.
18. Shrewsbury, G. D., "Numerical Study of a Research Circulation Control Airfoil Using Navier-Stokes Methods," Journal of Aircraft, Vol. 26, No. 1, pp.29-34, 1989.
19. Williams, S. L. and Franke, M. E., "Navier-Stokes Methods to Predict Circulation Control Airfoil Performance," Journal of Aircraft, Vol. 29, No.2, pp.243-249, March-April 1992.
20. th Aerospace Science Meeting, Reno, Nevada, AIAA paper 87-0100, Jan 12-15, 1987.
21. Oyler, T.E., and W.E. Palmer, "Exploratory Investigation of Pulse Blowing for Boundary Layer Control," North American Rockwell Report NR72H-12, Jan. 1972.