Optimization procedure for sailplane wing sections
Abstract eng: The article describes procedure of sailplane airfoil optimization with use of available numerical and experimental methods. Comments are given on calculation of boundary layer transition, integral parameters, measurement of maximum lift coefficient, visualization and flow control.
Contributors:
Publisher:
Institute of Theoretical and Applied Mechanics, AS CR, v.v.i., Prague
Conference Title:
Conference Title:
ENGINEERING MECHANICS 2006
Conference Venue:
Svratka (CZ)
Conference Dates:
2006-05-15 / 2006-05-18
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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