Airfoil boundary layer separation and control at low Reynolds numbers

Experiments in Fluids

Volumn 38, Issue 4, 2005, Pages 545-547

  Yarusevych, S ^a   Sullivan, P E ^a   Kawall, J G ^b  

^a UNIVERSITY OF TORONTO   (Canada)

^b RYERSON UNIVERSITY   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

ANEMOMETERS; BOUNDARY CONDITIONS; FLOW CONTROL; LAMINAR FLOW; PARAMETER ESTIMATION; PRESSURE MEASUREMENT; REYNOLDS NUMBER; SEPARATION; WIRE;

AIRFOIL PERFORMANCE; HOT-WIRE ANEMOMETRY; PERIODIC EXCITATION; SURFACE PRESSURE MEASUREMENTS;

AIRFOILS;

FLUID FLOW; REYNOLDS NUMBER;

EID: 17744383390     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00348-005-0943-2     Document Type: Article

References (4)

1. Lang M, Rist U, Wagner S (2004) Investigations on controlled transition development in a laminar separation bubble by means of LDA and PIV. Exp Fluids 36:43-52
2. Mueller TJ, DeLaurier JD (2003) Aerodynamics of small vehicles. Annu Rev Fluid Mech 35:89-111
3. Yarusevych S, Kawall JG, Sullivan PE (2003) Effect of acoustic excitation on airfoil performance at low Reynolds numbers. AIAA J 41:1599-1601
4. Zaman KBMQ (1992) Effect of acoustic excitation on stalled flows over an airfoil. AIAA J 30:1492-1499