Comparasion of stacionary and nonstacionary aerodynamic characteristics of the airfoil – results of the measurement in the wind tunnel
Abstract eng: This paper describes stacionary and nonstacionary measurement of aerodynamic characteristics of the airfoil in low speed wind tunnel on the University of Defence Brno. First part introduces the results for the airfoil in range of the angle of attack 0-360o with variable angle velocity. Further research focuses on experiments with high changes of the angle of attack with oscilations and variable frequences and amplitudes of motion.
Publisher:
Institute of Thermomechanics AS CR, v.v.i., Brno
Conference Title:
Conference Title:
ENGINEERING MECHANICS 2005
Conference Venue:
Svratka (CZ)
Conference Dates:
2005-05-09 / 2005-05-12
Rights:
Text je chráněný podle autorského zákona č. 121/2000 Sb.
Record appears in:
Record created 2014-11-12, last modified 2014-11-18
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