Unsteady measurements of aerodynamic characteristics of the airfoil
Abstract eng: This paper deals with unsteady measurements of aerodynamic characteristics of the symmetric airfoil for the angle of attack within the range from 0° to 360° with variable value of angular velocity. These results are processed for first and second revolution of airfoil NACA 0012 Mod. A special device was designed for these tests.
Publisher:
Institute of Theoretical and Applied Mechanics, AS CR, Prague
Conference Title:
Conference Title:
Engineering Mechanics 2012
Conference Venue:
Svratka (CZ)
Conference Dates:
12/05/2014 - 15/05/2014
Rights:
Text je chráněný podle autorského zákona č. 121/2000 Sb.
Record appears in:
Record created 2014-12-04, last modified 2014-12-04
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