VA-111 Shkval Rocket Performance Comparative Study with and without Supercavitation injection — Ep 01
VA-111 Shkval Rocket Performance Comparative Study with and without Supercavitation injection
- Lesson
- 01
- Run Time
- 13m
- Published
- Oct 17, 2026
- Category
- Aerodynamics & Aerospace
- Course Progress
- 0%
About This Lesson
- This problem simulates a VA-111 Shkval rocket using ANSYS Fluent software.
- The geometry is designed in SpaceClaim, and the meshing is performed using Fluent Meshing; the element number equals 257,000 polyhedral cells.
- The simulation uses the Pressure-based and VOF Multiphase model to define a two-phase flow.
- The turbulence model is set to SST k-ω.