क्यूआर कोड

Numerical Study of Shark-Skin Memetic Riblets on the Trailing Vortex and Boundary Layer Flow of the Wind Turbine Airfoil

Shark skin grooves, known to reduce hydrodynamic drag, have inspired riblet structures for flow control. This study investigates their application to airfoils, where flow separation at high angles of attack (AOA) compromises aerodynamic stability and wind turbine performance. Numerical simulations w...

पूर्ण विवरण

में बचाया:
मुख्य लेखकों: Xiaopei Yang, Renzhong Wang, Bin Zuo, Boyan Jiang
स्वरूप: Artigo
भाषा:Inglês
प्रकाशित: MDPI AG 2026-03-01
श्रृंखला:Fluids
विषय:
bionics
riblets
airfoil
unsteady numerical simulation
vortex suppression
ऑनलाइन पहुंच:https://www.mdpi.com/2311-5521/11/4/88
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