Results 71 to 80 of about 1,855 (186)

Optimization of High‑Speed WIG Airfoil with Consideration of Non‑ground Effect by a Two‑Step Deep Learning Inverse Design Method

open access: yesTransactions of Nanjing University of Aeronautics and Astronautics
Under complex flight conditions, such as obstacle avoidance and extreme sea state, wing-in-ground (WIG) effect aircraft need to ascend to higher altitudes, resulting in the disappearance of the ground effect.
WANG Chenlu   +6 more
doaj   +1 more source

Calculation and uncertainty analysis method for airfoil drag coefficient considering compressibility

open access: yesAIP Advances
In order to meet the need of evaluating the effectiveness of airfoil drag reduction design, the calculation and uncertainty analysis method for airfoil drag coefficient considering compressibility is studied.
Yufeng Du   +4 more
doaj   +1 more source

Airfoil Design Using Genetic Algorithms

open access: yes
Genetic algorithms (GAs) are a search method used in finding true or approximate solutions to optimization and search problems. They have been applied in different fields like computer science, engineering, and economics. Here, we apply GA to the problem of designing a symmetric airfoil with high lift coefficient. Each population member, or chromosome,
openaire   +2 more sources

Optimization of the double-slot blown airfoil with jet at the leading and trailing edges of the flap

open access: yesAIP Advances
An active lift augmentation technique combining trailing edge blowing and blown flap is explored in this study. A double-slot blown flap airfoil is designed based on NACA23015.
Songlin Xiang   +3 more
doaj   +1 more source

A novel approach to inverse design of wind turbine airfoils using tandem neural networks

open access: yesWind Energy
The performance of a wind turbine and its efficiency majorly depends on wind‐to‐rotor efficiency. The aerodynamic design of the wind turbine blades using high‐fidelity tools such as adjoint‐computational fluid dynamics (CFD) is accurate but ...
Apurva Anand   +3 more
doaj   +1 more source

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