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Journal Articles

Christopher S. Combs, E. Lara Lash, Phillip A. Kreth, and John D. Schmisseur.  "Investigating Unsteady Dynamics of Cylinder-Induced Shock-Wave/Transitional Boundary-Layer Interactions", AIAA Journal, Vol. 56 No. 4 (2018), pp. 1588-1599.

Christopher S. Combs, Phillip A. Kreth, John D. Schmisseur, and E. Lara Lash.  "Image-Based Analysis of Shock-Wave/Boundary-Layer Interaction Unsteadiness", AIAA Journal, Vol. 56, No. 3 (2018), pp. 1288-1293.

Conference Proceedings

2018 AIAA AVIATION Forum

Brian D. Kocher, Christopher S. Combs, Phillip A. Kreth, and John D. Schmisseur. "Investigation of the Streamwise Development of Distributed Surface Roughness Effects on Supersonic Flows", 2018 Fluid Dynamics Conference, AIAA AVIATION Forum, (AIAA 2018-4047)

2018 AIAA SciTech Forum

Christopher S. Combs, Stefen A. Lindörfer, Phillip A. Kreth, and John D. Schmisseur. "The Role of Boundary-Layer Thickness on Cylinder-Generated Shock-Wave/Turbulent Boundary-Layer Interactions, Part II: Experiments", 2018 AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, (AIAA 2018-0824)

Adam J. Harris, Phillip A. Kreth, Christopher S. Combs, and John D. Schmisseur. "Laser Differential Interferometry and Schlieren as an Approach to Characterizing Freestream Disturbance Levels", 2018 AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, (AIAA 2018-1100)

Kevin R. Holst, Ryan S. Glasby, Jon T. Erwin, Douglas L. Stefanski, Ryan B. Bond, and John D. Schmisseur. "High-Order Simulations of Shock Problems using HPCMP CREATE(TM)-AV Kestrel COFFE", 2018 AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, (AIAA 2018-1301)

Stefen A. Lindörfer, Christopher S. Combs, Ryan B. Bond, and John D. Schmisseur. "The Role of Boundary-Layer Thickness on Cylinder-Generated Shock-Wave/Turbulent Boundary-Layer Interactions, Part I: Computations", 2018 AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, (AIAA 2018-0380)

2017 AIAA AVIATION Forum

B. D. Kocher, C. S. Combs, P. A. Kreth, and J. D. Schmisseur. "Investigation of the Effects of Ablation-Induced Roughness on Supersonic Flows", 47th AIAA Fluid Dynamics Conference, AIAA AVIATION Forum, Denver, CO, June 2017

E. L. Lash, C. S. Combs, P. A. Kreth, and J. D. Schmisseur. "Study of the Dynamics of Transitional Shock Wave-Boundary Layer Interactions using Optical Diagnostics", 47th AIAA Fluid Dynamics Conference, AIAA AVIATION Forum, Denver, CO, June 2017

S. A. Lindörfer, C. S. Combs, P. A. Kreth, R. B. Bond, and J. D. Schmisseur. "Limiting Cases for Cylinder-Induced Shock Wave/Boundary Layer Interactions", 47th AIAA Fluid Dynamics Conference, AIAA AVIATION Forum, Denver, CO, June 2017

2017 AIAA SciTech Forum

E. L. Lash, C. S. Combs, P. A. Kreth, J. D. Schmisseur, "Experimental Investigation of a Cylinder-Induced Transitional Shock Wave-Boundary Layer Interaction", 55th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, Grapevine, TX, January 2017

S. A. Lindörfer, C. S. Combs, P. A. Kreth, J. D. Schmisseur, "Numerical Simulations of a Cylinder-Induced Shock Wave/Boundary Layer Interaction", 55th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, Grapevine, TX, January 2017

2016 AIAA AVIATION Forum

C. S. Combs, E. L. Lash, J. D. Schmisseur, "Investigation of a Cylinder-Induced Transitional Shock Wave-Boundary Layer Interaction using Laser Diagnostics", 32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Washington, D. C., June 2016

K. R. Holst, J. D. Schmisseur, "Reynolds-Averaged Navier-Stokes Simulations of Swept Shock Wave Boundary Layer Interactions at Mach 2 and 5", 46th AIAA Fluid Dynamics Conference, Washington, D. C., June 2016

E. L. Lash, C. S. Combs, P. A. Kreth, E. A. Beckman, J. D. Schmisseur, "Developing an Image-Based Analysis of the Dynamics of Transitional Shock Wave-Boundary Layer Interactions", 32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Washington, D. C., June 2016

S. A. Lindörfer, P. Anusonti-Inthra, C. S. Combs, P. A. Kreth, J. D. Schmisseur, "An Investigation of the Role of an Upstream Burst Diaphragm on Flow Quality within a Ludwieg Tube using RANS", 46th AIAA Fluid Dynamics Conference, Washington, D.C., June 2016