Control of Boundary Layer Transition on a Swept Wing by Suction.
نویسندگان
چکیده
منابع مشابه
Direct Numerical Simulation of Transition in a Swept-Wing Boundary Layer
Direct numerical simulation (DNS) is performed to examine laminar to turbulent transition due to high-frequency secondary instability of stationary crossflow vortices in a subsonic swept-wing boundary layer for a realistic natural-laminar-flow airfoil configuration. The secondary instability is introduced via inflow forcing derived from a two-dimensional, partial-differential-equation based eig...
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ژورنال
عنوان ژورنال: Journal of the Japan Society for Aeronautical and Space Sciences
سال: 2000
ISSN: 1344-6460
DOI: 10.2322/jjsass.48.393