Description
High power rocketry utilizes the engineering sciences to design rockets for speed or altitude performance goals. To accomplish these goals, rocket structures must be created with maximum strength and minimum mass. Using COMSOL Multiphysics, the aerodynamic loadings and composite structural stresses are simulated using supersonic CFD solvers and FSDT laminate shell simulations. These stress distribution simulations can inform the design, optimization, and manufacturing processes used to create high power rockets.
Details
Title
- Simulation of Composite Structures for High Power Rocket Applications
Contributors
- Terasaki, Brian (Author)
- Dong, Xiangyang (Thesis director)
- Murthy, Raghevandra (Committee member)
- Barrett, The Honors College (Contributor)
- Mechanical and Aerospace Engineering Program (Contributor)
Date Created
The date the item was original created (prior to any relationship with the ASU Digital Repositories.)
2024-12
Resource Type
Collections this item is in