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Aerospike Configurations' Effect on Aerodynamic Properties of Projectiles
Poster   Open access

Aerospike Configurations' Effect on Aerodynamic Properties of Projectiles

Julia Kondrat'yev and Kobi Menser
University of West Florida Libraries
Summer Undergraduate Research Program (University of West Florida, Pensacola, Florida, 08/2023)
10/14/2023

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Abstract

With the use of an inverted rocket nozzle design, called an aerospike, as the base of the projectile, the theory is that it creates a new method for designing supersonic projectiles, such as rifle bullets, that demonstrates a lowering in drag and significant improvements in their overall effectiveness.</br>Project Objectives:</br>1. Investigate the influence of projectile's physical properties on its aerodynamic characteristics. </br>2. Assess the degree of correspondence between the outcomes obtained from Computational Fluid Dynamics (CFD) models and experimental data during projectile analysis.</br>3. Determine the statistical evidence supporting a reduction in drag with the implementation of this projectile design.</br>The method of characteristics is employed in the design process to construct the Aerospikes tail end, leveraging the principles and insights derived from this theory.
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