NONSTACIONARY MEASUREMENT OF THE AIRFOIL AERODYNAMIC CHARACTERISTICS
Abstract eng: This paper describes nonstacionary measurement of the airfoil aerodynamic characteristics at 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 0-360° 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., Prague
Conference Title:
Conference Title:
Engineering Mechanics 2007
Conference Venue:
Svratka (CZ)
Conference Dates:
2007-05-14 / 2007-05-17
Rights:
Text je chráněný podle autorského zákona č. 121/2000 Sb.
Record appears in:
Record created 2014-10-24, last modified 2014-11-18
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