Full metadata
Title
Simulation of Composite Structures for High Power Rocket Applications
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.
Date Created
2024-12
Contributors
- Terasaki, Brian (Author)
- Dong, Xiangyang (Thesis director)
- Murthy, Raghevandra (Committee member)
- Barrett, The Honors College (Contributor)
- Mechanical and Aerospace Engineering Program (Contributor)
Topical Subject
Resource Type
Extent
23 pages
Copyright Statement
In Copyright
Primary Member of
Peer-reviewed
No
Open Access
No
Series
Academic Year 2024-2025
Handle
https://hdl.handle.net/2286/R.2.N.195376
System Created
- 2024-08-13 10:36:29
System Modified
- 2024-08-13 05:53:41
- 4 months 1 week ago
Additional Formats