Real-time optimization of wing drag and lift performance using a movable leading edge
EAR Camacho, MM da Silva, ARR Silva… - Physics of …, 2024 - pubs.aip.org
A real-time optimization strategy can provide any system with a considerable boost in
performance on the fly, which in real-world applications can be translated to lower energy …
performance on the fly, which in real-world applications can be translated to lower energy …
Influence of bioinspired morphing on the flow field characteristics of UAV wings at low Reynolds number
R Jini Raj, BR Rose J - Proceedings of the Institution of …, 2024 - journals.sagepub.com
The aerodynamic performance of unmanned aerial vehicles (UAV) can be improved by
optimizing the surface flow characteristics over a wide range of angle of attack (AoA) through …
optimizing the surface flow characteristics over a wide range of angle of attack (AoA) through …
NUMERICAL INVESTIGATION OF COOLING EFFECT OVER TWO-DIMENSIONAL AIRFOIL USING COLD AIR INJECTION TECHNIQUE
V Somashekar, SA Immanuel - International Journal of Fluid …, 2025 - dl.begellhouse.com
This numerical investigation delves into the cooling effects on a two-dimensional airfoil
subjected to low Reynolds number conditions using computational fluid dynamics …
subjected to low Reynolds number conditions using computational fluid dynamics …
Numerical Investigation of Cooling Effect Over 2D Airfoil using Cold Air Injection Technique
V SOMASHEKAR, I Selwynraj - International Journal of Fluid … - dl.begellhouse.com
This numerical investigation delves into the cooling effects on a two-dimensional airfoil
subjected to low Reynolds number conditions using computational fluid dynamics (CFD) …
subjected to low Reynolds number conditions using computational fluid dynamics (CFD) …
[PDF][PDF] Statistical modeling and predictive analysis of aerodynamic efficiency in NACA 2412 Airfoils: Engineering insights
This paper investigates the effects of varying the Angle of Attack (AoA) on the aerodynamic
efficiency of the NACA 2412 airfoil by analyzing the Lift-to-Drag (L/D) ratio. Using wind …
efficiency of the NACA 2412 airfoil by analyzing the Lift-to-Drag (L/D) ratio. Using wind …
[PDF][PDF] The Impact of Camber Variation on NACA 2412 Airfoil Efficiency and Its Implications for Adaptive Engineering Solutions
This paper investigates the effects of varying the camber on the aerodynamic efficiency of
the NACA 2412 airfoil by analyzing the Lift-to-Drag (L/D) ratio. Using wind tunnel tests at a …
the NACA 2412 airfoil by analyzing the Lift-to-Drag (L/D) ratio. Using wind tunnel tests at a …