High Reynolds number, multielement airfoil flowfield measurements

Journal of Aircraft

Volumn 37, Issue 3, 2000, Pages 499-507

  Spaid, Frank W ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; DRAG; LIFT; REYNOLDS NUMBER; TRANSPORT AIRCRAFT; WAKES;

FLAPS; MULTIELEMENT AIRFOILS;

AIRFOILS;

EID: 0033717051     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2626     Document Type: Article

References (13)

1. Valarezo, W. O., Dominik, C. J., McGhee, R. J., Goodman, W. L., and Paschal, K. B., "Multielement Airfoil Optimization for Maximum Lift at High Reynolds Number," AIAA Paper 91 -13332, Sept. 1991.
2. Lynch, F. T., "Experimental Necessities for Subsonic Transport Configuration Development," AIAA Paper 92-0158, Jan. 1992.
3. Nakayama, A., Kreplin, H. P., Morgan, H. L., "Experimental Investigation of Flowfield About a Multielement Airfoil," AIAA Journal, Vol. 28, No. 1, 1990, pp. 14-21.
4. Adair, D., and Home, W. C., "Turbulent Separated Flow in the Vicinity of a Single-Slotted Airfoil Flap," AIAA Paper 88-0613, Jan. 1988.
5. Chin, V. D., Peters, D. W., Spaid, F. W., and McGhee, R. J., "Flowfield Measurements About a Multi-Element Airfoil at High Reynolds Numbers," AIAA Paper 93-3137, July 1993.
6. Spaid, F. W., and Lynch, F. T., "High Reynolds Number, Multi-Element Airfoil Flowfield Measurements," AIAA Paper 96-0682, Jan. 1996.
7. Bertelrud, A., "Transition on a Three-Element High Lift Configuration at High Reynolds Numbers," AIAA Paper 98-0703, Jan. 1998.
8. McGinley, C. B., Anders, J., and Spaid, F. W., "Measurements of Reynolds Stress Profiles on a High-Lift Airfoil," AIAA Paper 98-2620, June 1998.
9. Lynch, F. T., Potter, R. C., and Spaid, F. W., "Requirements for Effective High-Lift CFD," International Council of the Aeronautical Sciences, Paper 96-2.7.1, Sept. 1996.
10. Ying, S. X., Spaid, F. W., McGinley, C. B., and Rumsey, C. L., "Investigation of Confluent Boundary Layers in High-Lift Flows," AIAA Paper 98-2622, June 1998.
11. Clauser, F. H., "Turbulent Boundary Layers in Adverse Pressure Gradients," Journal of the Aeronautical Sciences, Vol. 21, No. 2, 1954, pp. 91-108.
12. Klausmeyer, S. M., and Lin, J. C., "An Experimental Investigation of Skin Friction on a Multi-Element Airfoil," AIAA Paper 94-1870, June 1994.
13. Nakayama, A., Stack, J. P., Lin, J. C., and Valarzo, W. O., "Surface Hot-Film Technique for Measurements of Transition, Separation, and Reattachment Points," AIAA Paper 93-2918, July 1993.