Active control of flow separation from the slat shoulder of a supercritical airfoil

1st Flow Control Conference

Volumn , Issue , 2002, Pages

  Pack, Latunia G ^a   Schaeffler, Norman W ^a   Yao, Chung Sheng ^a   Seifert, Avi ^b,c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b TEL AVIV UNIVERSITY   (Israel)

^c ICASE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERO-DYNAMIC PERFORMANCE; CRUISE CONFIGURATION; INTEGRAL PARAMETERS; MOMENTUM COEFFICIENT; PARTICLE IMAGE VELOCIMETRIES; PERIODIC EXCITATIONS; SUPERCRITICAL AIRFOILS; TRAILING EDGE FLAPS;

ENERGY EFFICIENCY; FLOW CONTROL; FLOW SEPARATION; FLOW VISUALIZATION; NASA;

AIRFOILS;

EID: 84896693324     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

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3. McClean, J. D., Crouch, J. D., Stoner, R. C., Sakurai, S., Seidel, G. E., Feifel, W. M., and Rush, H. M., 'Study of the Application of Separation Control by Unsteady Excitation toCivil Transport Aircraft", NASA/CR-1999- 209338, 1999.
4. Lin J. C. and Dominik, C. J., "Parametric Investigation of a High-Lift Airfoil at High Reynolds Numbers", Journal of Aircraft, Vol. 33, No. 4, 1997, pp. 485-491.
5. Lin, J. C., Unpublished EET Data
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14. Bertelrud, A., "Transition on a Three-Element High Lift Configuration at High Reynolds Numbers", AIAA Paper 98-0703, January 1998.
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