Publikationsdatum:
2019-07-13
Beschreibung:
The linear stability of the laminar boundary layer on a swept flat plate with an imposed favorable pressure gradient was studied utilizing a linear stability model which accounts for streamline curvature for three-dimensional incompressible flows. Calculations were performed for a leading-edge sweep angle of 45 degrees and freestream valocity of 19 m/s. Computed disturbance amplification rates and wavelengths for stationary crossflow vortices were compared with available experimental results.
Schlagwort(e):
AERODYNAMICS
Materialart:
Instability and Transition; May 15, 1989 - Jun 09, 1989; Hampton, VA; United States
Format:
text
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