AIRFOIL MORPHING CONTROL AT LOW REYNOLDS NUMBER
Yusuf Thaer Fadel Yahia Elbadry;
Abstract
Micro Air Vehicles operates at low Reynolds number. The flight can be affected by very small disturbance and the flow can separate easily. New oscillating profile is proposed for oscillating the leading edge of NACA0012 airfoil. The incompressible Navier-Stokes equations are numerically solved using Galerkin/Least-Squares FEM.
Other data
| Title | AIRFOIL MORPHING CONTROL AT LOW REYNOLDS NUMBER | Other Titles | التحكم التشكلي لجنيح عند رقم رينولدز منخفض | Authors | Yusuf Thaer Fadel Yahia Elbadry | Issue Date | 2022 |
Attached Files
| File | Size | Format | |
|---|---|---|---|
| BB12092.pdf | 5.25 MB | Adobe PDF | View/Open |
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