Aerodynamic Drag Reduction in a Passenger Vehicle Using Rear-End Boat-Tail Geometry and a NACA 2310 Spoiler
Accepted at ICMDMSE 2026 · Springer Lecture Notes in Mechanical Engineering (Scopus / EI Compendex indexed)
I modelled a Toyota Innova in ANSYS Fluent and swept four boat-tail taper angles against seven spoiler angles of attack, 28 configurations in all, using steady RANS with the k-ε turbulence model at 40 m/s. A mesh-independence study backed the results. The best case, a 12° taper with a 12° spoiler, cut drag by about 14%.
- Solver
- ANSYS Fluent
- Model
- RANS k-ε
- Cases
- 4 × 7 = 28
- Best Cd
- 0.3268
- Drag
- 987 N → 849 N