Deep-learning-based aerodynamic shape optimization of rotor airfoils to suppress dynamic stall

J Liu, R Chen, J Lou, Y Hu, Y You - Aerospace Science and Technology, 2023 - Elsevier
The use of computational fluid dynamics (CFD) to optimize the aerodynamic shape of rotor
airfoils with the aim of suppressing dynamic stall is computationally expensive and …

Airfoils optimization based on deep reinforcement learning to improve the aerodynamic performance of rotors

J Liu, R Chen, J Lou, H Wu, Y You, Z Chen - Aerospace Science and …, 2023 - Elsevier
Airfoil optimization is the key to improving the aerodynamic performance of a rotor. However,
conventional optimization approaches cannot modify the airfoil shape intelligently in the way …

Parameter-based design and analysis of wind turbine airfoils with conformal slot co-flow jet

CY Ma, HY Xu - Journal of Applied Fluid Mechanics, 2022 - jafmonline.net
A co-flow jet (CFJ), an active flow control method combining blowing and suction control,
can effectively suppress the stall of airfoils. However, the streamwise jet channel along the …

Injection of micro jets to improve hydrodynamic performance of a ducted propeller

C Yang, HD Yao, C Sun, C Guo, C Wang, W Ren - Ocean Engineering, 2024 - Elsevier
In this study, micro jets were applied to actively controlling the flow of the international
standard ducted propeller model. The detached-eddy simulation (DES) method with the …

Experimental design for a novel co-flow jet airfoil

H Jiang, W Yao, M Xu - Advances in Aerodynamics, 2023 - Springer
Abstract The Co-flow Jet (CFJ) technology holds significant promise for enhancing
aerodynamic efficiency and furthering decarbonization in the evolving landscape of air …

[HTML][HTML] Helicopter performance enhancement by alleviating retreating blade stall using active flow control

TMT Soltan, MM Abdelrahman - Scientific African, 2023 - Elsevier
In this study, a model was created numerically to study the effect of active flow control on
helicopter blade to improve the retreating blade stall. Active flow control is applied to …

Separation Control for a Transonic Convex Corner Flow Using Ramp‐Type Vortex Generators

KC Su, KM Chung, S Isaev - International Journal of Aerospace …, 2022 - Wiley Online Library
A flap can be used to control wing camber and as a high‐lift device. A convex corner is a
simplified model of the upper surface of a flap. At transonic speeds, shock‐induced …

[HTML][HTML] 旋翼动态失速与反流流动控制研究进展

李国强, 赵鑫海, 易仕和, 宋奎辉, 赵光银 - 实验流体力学, 2023 - pubs.cstam.org.cn
直升机在大载荷高速前飞时, 旋翼桨叶桨距变化较大, 易发生动态失速; 后行桨叶内段旋转线速度
较低, 在来流叠加下形成反流区, 导致桨叶气动效率降低, 由此产生的桨叶疲劳失效和升力下降 …

Investigation of Helicopter Blade Tip Configuration during Hover Flight Employing Computational Fluid Dynamics

S Stouti, AT Lahlou, I Lagrat, H Mounir… - … and Simulation in …, 2024 - Wiley Online Library
Our research focused on investigating the influence of rotor blade tip geometry on the
aerodynamic performance of helicopters during hover flight, with the goal of enhancing …