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Carson Running

Carson Lee Running

Email: crunning@nd.edu

Phone: 507-390-1151

Office: B026 Hessert Laboratory

Education

M.S., University of Notre Dame, 2019

B.S., University of Notre Dame, 2015

Biography

Carson Running is a Graduate Research Assistant studying under the direction of Dr. Thomas Juliano. He received his B.S. and M.S. in Aerospace Engineering in 2015 and 2019, respectively. His scholarship is focused on hypersonic aerodynamics and aerothermodynamics with complementary interests in novel experimental surface-measurement techniques and facility design. Previously, he conducted research as a Student Summer Fellow in the Hypersonic Sciences Branch at the Air Force Research Laboratory under the direction of Dr. Roger Kimmel. Carson is a Graduate Associate for the Kaneb Center for Teaching and Learning at the University of Notre Dame, where he designs, prepares, and delivers workshops on effective teaching strategies and pedagogy for faculty, postdoctoral students, and graduate students. He is also a Graduate Fellow with the Research and Assessment for Learning (ReAL) Design Lab at the University of Notre Dame, where he conducts research to create predictive learning analytics and dynamic driven admissions criteria to better serve underprepared and underserved engineering students.

 

Selected Publications

C. L. Running, T. J. Juliano, J. S. Jewell, M. P. Borg, and R. L. Kimmel, “Characterization of Post-Shock Thermal Striations on a Cone/Flare” AIAA Journal, Submitted – Under Review

C. L. Running, T. J. Juliano, J. S. Jewell, M. P. Borg, and R. L. Kimmel, “Hypersonic Shock-Wave/Boundary-Layer Interactions on a Cone/Flare” Experimental Thermal and Fluid Science, Vol. 109

E. M. Hoberg, C. Huffman, N. Sanchez-Plesha, C. L. Running, N. Kato, S. Im, and T. J. Juliano, “Flow Characterization of a Supersonic and Hypersonic Arc-Heated Wind Tunnel”, AIAA Paper 2019-3093, June 2019. doi:10.2514/6.2019-3093

C. L. Running, H. Sakaue, and T. J. Juliano, “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

C. L. Running, T. J. Juliano, J. S. Jewell, M. P. Borg, and R. L. Kimmel, “Hypersonic Shock-Wave/Boundary-Layer Interactions on a Cone/Flare Model”, AIAA Paper 2018-3702, June 2018. doi:10.2514/6.2018-3702

C. L. Running, M. J. Thompson, T. J. Juliano, and H. Sakaue, “Boundary-layer Separation Detection for a Cone at High Angle of Attack in Mach 4.5 Flow with Pressure-Sensitive Paint”, AIAA Paper 2017-3120, June 2017. doi:10.2514/6.2017-3120

 

Summary of Activities/Interests

  • Shock-Wave/Boundary-Layer Interactions
  • Boundary-Layer Transition and Instability
  • Boundary-Layer Separation and Reattachment
  • Global Surface Pressure and Temperature Measurement Techniques
  • Hypersonic Facility Design and Characterization
  • Learning Sciences and Analytics
  • Teaching Pedagogy

 

Adviser(s)