Enhancing aerodynamic efficiency is vital for optimizing aircraft performance and operational effectiveness. It enables greater speeds and reduced fuel consumption, leading to lower operating costs. Hence, the implementation of Gurney flaps represents a promising avenue for improving airfoil aerodynamics. The optimization of Gurney flaps holds considerable ramifications for improving the lift and stall characteristics of airfoils in aircraft and wind turbine blade designs. The efficacy of implementing Gurney flaps hinges significantly on its design parameters, namely, flap height and mounting angle. This study attempts to optimize these parameters using a design optimization framework, which incorporates training a Radial Basis Function surrogate model based on CFD data from two-dimensional (2D) Reynolds-Averaged Navier-Stokes (RANS) simulations. The Cuckoo Search algorithm is then employed to obtain the optimal design parameters and compared with other competing optimization algorithms. The optimized Gurney flap configuration shows a notable improvement of 10.28% in
"Tyagi, A., Singh, P., Rao, A., Kumar, G. and Singh, R.K., 2023. A Novel Framework for Optimizing Gurney Flaps using RBF Neural Network and Cuckoo Search Algorithm." arXiv preprint arXiv:2307.13612.
Short summary of the minimal requirements:
Note: all other necessary build tools and dependencies are shipped with the source code or are downloaded automatically.
- In case, you do not have the required dependencies, kindly install using the following code
pip install -r requirements.txt
- If you have these dependenies installed, you can create a local repository by cloning the repository:
git clone https://github.com/GipsyOmega/Surrogate-Metaheuristics.git
- Run the project using
python CSASurrogate.py
This research paper/project is conducted under the Fluid Mechanics Group of Delhi Technological University, supervised by Prof. Raj Kumar Singh.