The repository contains the results of studies on two wings with Clark Y and Selig S1223 airfoil profiles. The wings were modified by integrating sprayers mounted on their lower surface in five configurations: single sprayer at the leading edge (A), single sprayer at mid-chord (B), double sprayers at the leading edge (C), double sprayers at mid-chord (D), and asymmetric double sprayers (E). Reference cases are marked with the suffix “smooth.” Three sprayers differing in geometry were analyzed: 6MS (Agroplast 6MS 05P2), 8MS (Agroplast 8MS 110 05P2), and ID (Lechler ID-120-05).
1. Archive file “WT”: Contains 160 CSV files with the results of experimental wind tunnel tests. The archive includes folders and subfolders specifying the investigated configuration, determined by: airfoil type, sprayer type, sprayer arrangement, and airflow velocity expressed in m/s.
2. Archive file “CFD”: Contains 64 CSV files with the results of numerical simulations performed using computational fluid dynamics (CFD) in Ansys Fluent. The archive includes folders and subfolders specifying the investigated configuration, determined by: airfoil type, sprayer type, sprayer arrangement, and airflow velocity expressed in m/s.
3. Archive file “CAD”: Contains CAD models of the tested objects, including sprayers with nuts, wings with slots, and example computational domains for numerical simulations.
(2025)