METHOD FOR OPTIMIZING BALLISTIC MISSILE PERFORMANCE

Abstract

ABSTRACT A method (100) for optimizing ballistic missile performance. Further, the method comprising creating a detailed CAD model of the missile with key design features. Further, the method (100) comprising the steps of performing CFD simulations using ANSYS Workbench Fluent with varied boundary conditions. Further, the method (100) comprising the steps of generating a fine mesh of the CAD model to capture flow phenomena. Further, the method (100) comprising the steps of analyzing performance metrics such as trajectory stability and aerodynamic efficiency. Further, the method (100) comprising the steps of identifying optimal design configurations to enhance missile effectiveness.

Specification

Description:FIELD OF THE DISCLOSURE
[0001] This invention generally relates to the field of aerospace engineering and, in particular, to a method for optimizing the performance of ballistic missiles through advanced computational fluid dynamics simulations and design modifications aimed at enhancing aerodynamic efficiency and operational effectiveness.
BACKGROUND
[0002] The subject matter discussed in the background section should not be assumed to be prior art merely as a result of its mention in the background section. Similarly, a problem mentioned in the background section or associated with the subject matter of the background section should not be assumed to have been previously recognized in the prior art. The subject matter in the background section merely represents different approaches, which in and of themselves may also correspond to implementations of the claimed technology.
[0003] The performance of ballistic missiles is critically influenced by their aerodynamic design and stability during flight. Tradi , Claims:WE CLAIM:
1. A method (100) for optimizing ballistic missile performance, the method comprising the steps of:
creating a detailed CAD model of the missile with key design features;
performing CFD simulations using ANSYS Workbench Fluent with varied boundary conditions;
generating a fine mesh of the CAD model to capture flow phenomena;
analyzing performance metrics such as trajectory stability and aerodynamic efficiency; and
identifying optimal design configurations to enhance missile effectiveness.

2. The method (100) as claimed in claim 1, wherein the CAD model includes a modified fin configuration with three fins instead of the conventional four fins to improve aerodynamic performance.

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