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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Aerospike Configurations' Effect on Aerodynamic Properties of Projectiles2.32 MBDownloadView
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Title
Aerospike Configurations' Effect on Aerodynamic Properties of Projectiles
Resource Type
Poster
Event
Summer Undergraduate Research Program (University of West Florida, Pensacola, Florida, 08/2023)
Contributors
John Sutz (Faculty Mentor)
Publisher
University of West Florida Libraries; Argo Scholar Commons
Format
pdf
Copyright
Permission granted to the University of West Florida Libraries to digitize and/or display this item for non-profit research and educational purposes. Any reuse of this item in excess of fair use or other copyright exemptions requires the permission of the copyright holder.
Identifiers
99380472265806600
Academic Unit
Summer Undergraduate Research Program 2023; Mechanical Engineering; Hal Marcus College of Science and Engineering
Language
English
Aerospike Configurations' Effect on Aerodynamic Properties of Projectiles