Python Coding for Flapping Wing Aerodynamics
Budget: ₹1,500 – ₹12,500 INR
I am seeking a proficient Python developer with a strong background in aerospace engineering and numerical methods, specifically the Unsteady Vortex Lattice Method (UVLM). The task is to create a code that can analyze the aerodynamics of foldable flapping wings, with a focus on lift and drag forces. The primary application of this project is in aerospace research.
Key Requirements:
- Expertise in Python programming
- In-depth understanding of aerodynamics, particularly lift and drag forces
- Experience with the Unsteady Vortex Lattice Method
- Aerospace engineering background
I have detailed data available for the flapping wing design, which will be provided upon project commencement. The ideal freelancer will be able to not only develop the code, but also provide insights based on the analysis of the results.
References:
1. Verstraete, M. L., Roccia, B. A., Mook, D. T., & Preidikman, S. (2019). A co-simulation methodology to simulate the nonlinear aeroelastic behavior of a folding-wing concept in different flight configurations. Nonlinear Dynamics, 98, 907-927.
2. Verstraete, M. L., Preidikman, S., Roccia, B. A., & Mook, D. T. (2015). A numerical model to study the nonlinear and unsteady aerodynamics of bioinspired morphing-wing concepts. International Journal of Micro Air Vehicles, 7(3), 327-345.
Key Requirements:
- Expertise in Python programming
- In-depth understanding of aerodynamics, particularly lift and drag forces
- Experience with the Unsteady Vortex Lattice Method
- Aerospace engineering background
I have detailed data available for the flapping wing design, which will be provided upon project commencement. The ideal freelancer will be able to not only develop the code, but also provide insights based on the analysis of the results.
References:
1. Verstraete, M. L., Roccia, B. A., Mook, D. T., & Preidikman, S. (2019). A co-simulation methodology to simulate the nonlinear aeroelastic behavior of a folding-wing concept in different flight configurations. Nonlinear Dynamics, 98, 907-927.
2. Verstraete, M. L., Preidikman, S., Roccia, B. A., & Mook, D. T. (2015). A numerical model to study the nonlinear and unsteady aerodynamics of bioinspired morphing-wing concepts. International Journal of Micro Air Vehicles, 7(3), 327-345.