Is this project an undergraduate, graduate, or faculty project?
Undergraduate
Project Type
group
Campus
Daytona Beach
Authors' Class Standing
Massimo Mansueto, Freshman Andres Torres-Figueroa, Graduate student
Lead Presenter's Name
Massimo Mansueto
Lead Presenter's College
DB College of Engineering
Faculty Mentor Name
Dr. Michael Kinzel
Abstract
The Generalized Cloud-Based Compressible Aerodynamics Calculator and Simulation Web App focuses on the development of a tool to support the analysis, visualization, and teaching of compressible aerodynamics. In the case of most undergraduate aerospace engineering courses, students rely on static equations, charts, and manual calculations, which can make it difficult to conceptualize complex flow phenomena such as shock waves, expansion fans, and nozzle flow. The purpose of this project is to create an accessible platform that integrates a compressible flow calculator, nozzle sizing tool, and interactive simulations into a single educational resource. The application is implemented using modern web development technologies such as Cloudfare, Python, and an open-source project to ensure cross-platform accessibility and the ease of integration into classroom environments. By leveraging cloud deployment, the tool enables real-time computation and graphical visualization without requiring local software installation allowing for ease of use. The project is currently in a proof-of-concept stage, with several core computational modules and graphing capabilities already functional. Ongoing development includes refinement of the user interface, expansion of simulation features, and collaboration with faculty to align the platform with curriculum needs. Preliminary results demonstrate that the web-based approach can streamline repetitive calculations and provide intuitive visual feedback, improving both efficiency and conceptual understanding. The anticipated outcome is a publicly accessible educational tool that standardizes computational methods in compressible aerodynamics while enhancing student engagement through interactive learning and visual simulation.
Did this research project receive funding support (Spark, SURF, Research Abroad, Student Internal Grants, Collaborative, Climbing, or Ignite Grants) from the Office of Undergraduate Research?
No
Included in
Aerodynamics and Fluid Mechanics Commons, Engineering Education Commons, Software Engineering Commons
Generalized Cloud-Based Compressible Aerodynamics Calculator and Simulation Web App
The Generalized Cloud-Based Compressible Aerodynamics Calculator and Simulation Web App focuses on the development of a tool to support the analysis, visualization, and teaching of compressible aerodynamics. In the case of most undergraduate aerospace engineering courses, students rely on static equations, charts, and manual calculations, which can make it difficult to conceptualize complex flow phenomena such as shock waves, expansion fans, and nozzle flow. The purpose of this project is to create an accessible platform that integrates a compressible flow calculator, nozzle sizing tool, and interactive simulations into a single educational resource. The application is implemented using modern web development technologies such as Cloudfare, Python, and an open-source project to ensure cross-platform accessibility and the ease of integration into classroom environments. By leveraging cloud deployment, the tool enables real-time computation and graphical visualization without requiring local software installation allowing for ease of use. The project is currently in a proof-of-concept stage, with several core computational modules and graphing capabilities already functional. Ongoing development includes refinement of the user interface, expansion of simulation features, and collaboration with faculty to align the platform with curriculum needs. Preliminary results demonstrate that the web-based approach can streamline repetitive calculations and provide intuitive visual feedback, improving both efficiency and conceptual understanding. The anticipated outcome is a publicly accessible educational tool that standardizes computational methods in compressible aerodynamics while enhancing student engagement through interactive learning and visual simulation.