MR-CFD ANSYS Fluent Tutorials and Services

ANSYS Discovery: NLAW Parametric Drag Optimization of Nose Geometry, CFD Simulation

Unsteady aerodynamics isn’t just for aircraft – it’s now a key part of modern missile and launcher design as well.​ In our latest MR CFD training package, we’ve simulated the aerodynamic behavior of the NLAW launcher nose in ANSYS Discovery at an inlet velocity of 120 m/s to visualize how pressure and velocity actually distribute over the system under operating conditions. This CFD study helps engineers:​ Identify critical low‑ and high‑pressure regions on the launcher nose that can impact stability and structural integrity.​ Detect separation and recirculation zones in the wake that contribute directly to drag and potential control issues.​ Quantify aerodynamic loads on the launcher surfaces to support safer and more efficient design decisions.​ What you get in this package:​ 3D geometry of the NLAW launcher prepared in ANSYS Discovery (ready to modify and reuse). Mesh file and full CFD setup for the aerodynamic analysis case. A step‑by‑step Fluent/Discovery training video, so you can follow the entire workflow from geometry to post‑processing and results interpretation. If you are working in defense, aerodynamics, or advanced weapon system design and want a practical CFD case to learn from or adapt, this project gives you a complete, ready‑to‑run template.​ 🔗 Project link: ANSYS Discovery – Aerodynamic Analysis of NLAW Nose Design (CFD Simulation) #CFD #ANSYS #AnsysDiscovery #Aerodynamics #NLAW #MissileDesign #DefenseEngineering #MRCFD