An experimental investigation of wake development in arbitrary pressure gradients

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Liu, Xiaofeng ^a   Thomas, Flint O ^a   Nelson, Robert C ^a  

^a UNIVERSITY OF NOTRE DAME   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; PRESSURE GRADIENT; TURBULENCE; WIND TUNNELS;

EXPERIMENTAL INVESTIGATIONS; FAVORABLE PRESSURE GRADIENTS; HIGH LIFT SYSTEM; IMPOSED PRESSURE GRADIENT; SPLITTER PLATES; THREE COMPONENT; UNIQUE FEATURES; VELOCITY DEFECTS;

WAKES;

EID: 84982318970     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-677     Document Type: Conference Paper

References (19)

1. Garner, P.L, Meredith, P. T., and Stoner, R. C., "Areas for CFD Development as Illustrated by Transport Aircraft Applications", AIAA paper 91-1527, 1991.
2. Mack, M.D., and McMasters, J. H., 1992, "High Reynolds Number Testing in Support of Transport Airplane Development", AIAA paper 92-3982.
3. Lin, J.C., Robinson, S.K., and McGhee, R.J., "Separation Control on High Reynolds number Multi-Elemnet Airfoils", AIAA paper 92-2636, 1992.
4. Smith, A.M.O., 1975, "High-Lift Aerodynamics", AIAA Journal of Aircraft, 12, 6, pp 501-530.
5. Petrov, A.V., "Certain Types of Separated Flow over Slotted Wings", Fluid Mechanics-Soviet Research, Vol. 7, No.5, September-October 1978, pp 80-89.
6. Chin, V.D., Peters, D.W., Spaid, F.W. and McGhee, R.J., 1993, "Flowfield Measurements About a Multi-Element Airfoil at High Reynolds Numbers", AIAA paper 93-3137.
7. Hill, P.G., Schaub, U.W., and Senoo, Y., "Turbulent Wakes in Pressure Gradients", Journal of Applied Mechanics, Vol. 30, No. 12 (December 1963), pp 518-524.
8. Zhou, M. D. and Squire, L. C, 1985, "The Interaction of a Wake with a Turbulent Boundary Layer", Aeronautical Journal, pp 72-81.
9. Hoffenberg, R, Sullivan, J.P., and Schneider, S.P., "Wake Measurements in a Strong Adverse Pressure Gradient", AIAA Paper 95-1912, June 1995.
10. Roos F.W., "Experimental Studies of Wake Retardation in a Simulated High-Lift system Flow Field", AIAA Paper 97-1813, June 1997.
11. Narasimha, R., and Prabhu, A., "Equilibrium and Relaxation in Turbulent Wakes", Journal of Fluid Mechanics, (1972), vol.54, parti, pp 17.
12. Prabhu, A., and Narasimha, R., "Turbulent Non-equilibrium Wakes", Journal of Fluid Mechanics, (1972), vol.54, parti, pp 19-38.
13. Hoffenberg, R. and Sullivan, J.P., "Measurement and Simulation of a Decelerated Wake", AIAA Paper 98-0522, January 1998.
14. Klebanoff, P.S., "Characteristics of turbulence in a boundary layer with zero pressure gradient", NACA TN 3178, July 01, 1954.
15. Schlichting, H., "Boundary Layer Theory", McGraw-Hill Book Company, Sixth Edition, 1968.
16. Thomas, F.O., Liu, X., and Nelson, R.C., "Experimental Investigation of the Confluent Boundary Layer of a High-lift System", AIAA paper 97-1934, 1997.
17. Ramaprian, B.R., and Patel, V.C., "The symmetric Turbulent Wake of a Flat Plate", AIAA journal, September 1982, Vol. 20, No.9, pp l228-1235.
18. Andereopoulos, J., and Bradshaw, P., 1980, "Measurements of Interacting Turbulent Shear layers in the near Wake of a Flat Plate", Journal of Fluid Mechanics, vol. 100, part 3, pp 639-668.
19. Chevray, R. and Kovasznay, L.S.G., 1969, "Turbulence Measurements in the Wake of a Thin Flat Plate", AIAA Journal, vol. 7, pp 1641-1643.