Enhanced performance of airfoils at moderate mach numbers using zero-mass flux pulsed blowing

39th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2001, Pages

  Hites, Michael ^a   Nagib, Hassan ^a   Bachar, Tomer ^b   Wygnanski, Israel ^b  

^a ILLINOIS INSTITUTE OF TECHNOLOGY   (United States)

^b TEL AVIV UNIVERSITY   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; AIRFOILS; ANGLE OF ATTACK; DRAG; MACH NUMBER;

ANGLES OF ATTACK; COMPRESSIBILITY EFFECTS; FORCING FREQUENCIES; LIFT COEFFICIENT; LIFT ENHANCEMENT; MAXIMUM PRESSURE; PRESSURE COEFFICIENT DISTRIBUTION; SEPARATION CONTROL;

LIFT;

EID: 85088185756     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-734     Document Type: Conference Paper

References (22)

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