Directory
Carson L. Running
Assistant Professor
Full-Time Faculty
School of Engineering: Department of Mechanical and Aerospace Engineering
Bio
Professor Running works to motivate students inside and outside of the classroom to make a positive difference in the world. Prof. Running's technical scholarship is focused on hypersonic aerodynamics and aerothermodynamics with complementary interests in novel experimental surface-measurement techniques and facility design. These research endeavours seek to deliver answers to fundamental questions facing the hypersonic community and will lead to increased national security, space exploration and a revolutionized commercial-flight industry providing flights from LA to Tokyo in under 2 hours. Prof. Running is also active in pedagogical educational research, where he investigates predictive learning analytics and dynamic driven admissions criteria to better serve underprepared and underserved students.
Selected Publications
- Running, C. L., & Juliano, T. J. (2021). Global skewness and coherence for hypersonic shock-wave/boundary-layer interactions with pressure-sensitive paint. Aerospace – Special Issue: Hypersonics: Emerging Research, 8(5), 1-14. doi: 10.3390/aerospace8050123
- Running, C. L., & Juliano, T. J. (2021). Global measurements of hypersonic shock-wave/boundary-layer interactions with pressure-sensitive paint. Experiments in Fluids – Topical Collection: The Fluid Mechanics of Hypersonic Flight, 62(91), 1-18. doi:10.1007/s00348-021-03194-8
- Running, C. L., Juliano, T. J., Borg, M. P., & Kimmel, R. L. (2020). Characterization of post-shock thermal striations on a cone/flare. AIAA Journal, 58(5), 2352-2358. doi:10.2514/1.J059095
- Running, C. L., Juliano, T. J., Jewell, J. S., Borg, M. P., & Kimmel, R. L. (2020). Hypersonic shock-wave/boundary-layer interactions on a cone/flare. Experimental Thermal and Fluid Science, 109(109911), 19. doi:10.1016/j.expthermflusci.2019.109911
- Running, C. L., Sakaue, H., and Juliano, T. J., Hypersonic boundary-layer separation detection with pressure-sensitive paint for a cone at high angle of attack Experiments in Fluids, Vol. 60, No. 23, 2019, pp. 1-13. doi:10.1007/s00348-018-2665-2
Degrees
- Ph.D. aerospace engineering, University of Notre Dame, 2020
- M.S. aerospace engineering, University of Notre Dame, 2019
- B.S. aerospace engineering, University of Notre Dame, 2015
Courses Taught
- Fluid Mechanics (MEE 308)
- Compressible Flow (AEE 553)
Research Interests
- Shock-wave/boundary-layer interactions
- Boundary-layer transition and instability mechanisms
- Boundary-layer separation and reattachment
- Global surface pressure and temperature measurement techniques
- Hypersonic facility design and characterization
- Learning sciences and analytics
- Teaching pedagogy