Man Portable Anti Tank Missiles Training Package: 6 Projects by ANSYS Discovery

$2,000.00 $1,400.00 Internship

  • 6 Anti Tank Missiles Projects By ANSYS Discovery.
  • Javelin and NLAW Parametric Optimization Of Tail Fin and Nose Cone.
  • Flight Path Deviation Analysis of Anti Tank Missiles By ANSYS Discovery.
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ANSYS Discovery: NLAW Flight Path Deviation Analysis, CFD Simulation

  • Parametric CFD analysis of NLAW fin angles (1°-25°).
  • 3D flight path deviation from the straight-line trajectory for each fin incidence angle.
  • Pitch and Yaw deviation of NLAW missile.

ANSYS Discovery: Javelin Nose Cone Parametric Aerodynamic Analysis, CFD Simulation

  • Real-time parametric CFD exploration of Javelin missile nose cone geometry using ANSYS Discovery
  • Instantaneous drag and pressure analysis across multiple nose profiles of Javelin via History Tracking
  • GPU-accelerated aerodynamic screening of Javelin missile without manual remeshing or solver restarts

ANSYS Discovery: Javelin Tail Fin Configuration Analysis, CFD Simulation

  • Parametric CFD analysis of Javelin missile tail fin count and geometry.
  • Aerodynamic comparison of fin span and chord length of Javelin without manual remeshing.
  • Javelin Instantaneous drag and flow stability evaluation across multiple fin configurations via History Tracking

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

  • Distinct pressure distributions across nose configurations in ANSYS Discovery CFD analysis
  • NLAW blunt nose exhibits largest stagnation zone, optimized for shaped charge performance
  • Ogive profiles show focused high-pressure regions with potential drag benefits
  • Parametric Rapid Design of NLAW nose in ANSYS Discovery explore mode

ANSYS Discovery: Javelin Aerodynamic Control Analysis, CFD Simulation

  • Flight path deviation angles (θ and φ) calculation to assess Javelin missile maneuverability in 3D space.
  • Parametric CFD analysis of Javelin tail fin deflection (0°–25°) via ANSYS Discovery History Tracking.
  • Optimal control window identification based on force efficiency, drag penalty, and directional stability.
  • 3D force vector extraction (Fx, Fy, Fz) and lateral force evaluation across all configurations without manual remeshing.

ANSYS Discovery: NLAW Aerodynamic Analysis, CFD simulation

  • 3D Modeling and Geometry Preparation of NLAW in ANSYS Discovery
  • Aerodynamic Analysis
  • CFD Simulation of NLAW in ANSYS Discovery

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If you need the Geometry designing and Mesh generation training video for one product, you can choose this option.
editable geometry and mesh allows users to create and modify geometry and mesh to define the computational domain for simulations.
The case and data files in ANSYS Fluent store the simulation setup and results, respectively, for analysis and post-processing.
Geometry, Mesh, and CFD Simulation methodologygy explanation, result analysis and conclusion
Enhancing Your Project: Comprehensive Consultation and Optimization Services
The MR CFD certification can be a valuable addition to a student resume, and passing the interactive test can demonstrate a strong understanding of CFD simulation principles and techniques related to this product.
The journal file in ANSYS Fluent is used to record and automate simulations for repeatability and batch processing.

Description

1. Introduction

Nowadays, Man Portable Anti Tank Missiles play a crucial and decisive role in direct combat. The ability to destroy enemy tanks with a small, portable weapon greatly increases the effectiveness and importance of this class of weapons. Among the most well-known anti-armor systems in this category are the Javelin and NLAW, which are similar in principle of operation but differ in certain features such as range and reusability.

2. Objectives

What you will see in this training package is an exceptional use of the real-time simulation capabilities of ANSYS Discovery for Anti Tank Missiles. We use features such as Parametric Design to instantly evaluate the impact of Tail Fin Configuration and Nose Cone Configuration on the aerodynamics of these weapons, as well as their Flight Path Deviation.

3. Summary

After reviewing this training package, you will realize the undeniable importance of design and of seeing the immediate impact of design changes in simulation results. For example, in the table shown, we extracted the results of changing the tail fin angle of the Javelin and observed how each degree of change produces a certain amount of deviation in the weapon’s direction of travel.

Anti Tank Missiles

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