UDF Development for Flapping Wing Aerodynamics
Budget: ₹1,500 – ₹12,500 INR
I'm looking for an expert who can develop a User Defined Function (UDF) in ANSYS Fluent for analyzing the aerodynamic performance of a foldable flapping wing. The project should be completed within a week.
Key Focus:
- The primary focus is on the aerodynamic performance of the wing.
- Critical parameters for analysis include lift and drag forces, as well as flow patterns around the wings.
Refer:
Reference: Guerrero, J. E., Pacioselli, C., Pralits, J. O., Negrello, F., Silvestri, P., Lucifredi, A., & Bottaro, A. (2016). Preliminary design of a small-sized flapping UAV: I. Aerodynamic performance and static longitudinal stability. Meccanica, 51, 1343-1367.
Video: https://www.youtube.com/watch?v=Ea2sPb4_HIE
Refer above, before confirming your bids.
Requirements:
- The analysis should be done with high in accuracy; it needs to be perfect but should be reliable.
- Only experienced candidates who can develop UDFs in ANSYS should apply. Please do not waste my time if you lack this expertise.
Key Focus:
- The primary focus is on the aerodynamic performance of the wing.
- Critical parameters for analysis include lift and drag forces, as well as flow patterns around the wings.
Refer:
Reference: Guerrero, J. E., Pacioselli, C., Pralits, J. O., Negrello, F., Silvestri, P., Lucifredi, A., & Bottaro, A. (2016). Preliminary design of a small-sized flapping UAV: I. Aerodynamic performance and static longitudinal stability. Meccanica, 51, 1343-1367.
Video: https://www.youtube.com/watch?v=Ea2sPb4_HIE
Refer above, before confirming your bids.
Requirements:
- The analysis should be done with high in accuracy; it needs to be perfect but should be reliable.
- Only experienced candidates who can develop UDFs in ANSYS should apply. Please do not waste my time if you lack this expertise.