College
College of Engineering
Department
Mechanical and Aerospace Engineering Department
Faculty Mentor
Doug Hunsaker
Abstract
Hypersonic (at least 5 times faster than sound waves can travel) aircraft are quickly becoming a solution for fast travel for commercial and defense purposes.
Document Type
Poster
Publication Date
2-20-2025
Recommended Citation
Wiberg, Jacob, "Arrowhead-Shaped Shock Angle Influence Leading Edge Equation Influence Aircraft Outperform Other Structures at Hypersonic Speeds" (2025). Research on Capitol Hill. Paper 161.
https://digitalcommons.usu.edu/roch/161