Flow transients induced on a 2D airfoil by pulse-modulated actuation

Experiments in Fluids

Volumn 40, Issue 2, 2006, Pages 329-331

  Amitay, Michael ^a   Glezer, Ari ^b  

^a RENSSELAER POLYTECHNIC INSTITUTE   (United States)

^b GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRFOILS; AMPLITUDE MODULATION; ANEMOMETERS; FLOW VISUALIZATION; JETS; PULSE MODULATION; RESONANCE; VORTEX FLOW;

HOT-WIRE ANEMOMETRY; PULSE-MODULATED ACTUATION; RESONANT WAVEFORM;

FLOW OF FLUIDS;

ACTUATORS; AIRFOILS; AMPLITUDE MODULATION; ANEMOMETERS; FLOW OF FLUIDS; FLOW VISUALIZATION; JETS; PULSE MODULATION; RESONANCE; VORTEX FLOW;

EID: 31144451800     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00348-005-0069-6     Document Type: Article

References (7)

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2. Amitay M, Glezer A (2002) Controlled transients of flow reattachment over stalled airfoils. Int J Heat Trans Fluid Flow 23(5): 690-699
3. Amitay M, Smith DR, Kibens V, Parekh DE Glezer A (2001) Modification of the aerodynamics characteristics of an unconventional airfoil using synthetic jet actuators. AIAA J 39(3):361-370
4. Ahuja KK, Burrin RH (1984) Control of flow separation by sound. AIAA 84-2298
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6. Seifert A, Darabi A, Wygnanski I (1996) Delay of airfoil stall by periodic excitation. J Aircraft 33(4):691-698
7. Wu JZ, Lu XY, Denny AG, Fan M Wu JM (1998) Post-stall control on an airfoil by local unsteady forcing. J Fluid Mech 371:21-58