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Phillip A. Kreth

University of Tennessee

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Publication

Featured researches published by Phillip A. Kreth.

32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference | 2016

Developing an Image-Based Analysis of the Dynamics of Transitional Shock Wave-Boundary Layer Interactions

E. Lara Lash; Christopher S. Combs; Phillip A. Kreth; Emily A. Beckman; John D. Schmisseur

55th AIAA Aerospace Sciences Meeting | 2017

Experimental Investigation of a Cylinder-Induced Transitional Shock Wave-Boundary Layer Interaction

E. L. Lash; Christopher S. Combs; Phillip A. Kreth; John D. Schmisseur

55th AIAA Aerospace Sciences Meeting | 2017

Numerical Simulations of a Cylinder-Induced Shock Wave/Boundary Layer Interaction

Stefen A. Lindörfer; Christopher S. Combs; Phillip A. Kreth; John D. Schmisseur

47th AIAA Fluid Dynamics Conference | 2017

Study of the Dynamics of Transitional Shock Wave-Boundary Layer Interactions using Optical Diagnostics

E. Lara Lash; Christopher S. Combs; Phillip A. Kreth; John D. Schmisseur

47th AIAA Fluid Dynamics Conference | 2017

Limiting Cases for Cylinder-Induced Shock Wave/Boundary Layer Interactions

Stefen A. Lindörfer; Christopher S. Combs; Phillip A. Kreth; Ryan B. Bond; John D. Schmisseur

AIAA Journal | 2017

Image-Based Analysis of Shock-Wave/Boundary-Layer Interaction Unsteadiness

Christopher S. Combs; Phillip A. Kreth; John D. Schmisseur; E. Lara Lash

47th AIAA Fluid Dynamics Conference | 2017

Investigation of the Effects of Ablation-Induced Roughness on Supersonic Flows

Brian D. Kocher; Christopher S. Combs; Phillip A. Kreth; John D. Schmisseur

AIAA Journal | 2018

Investigating Unsteady Dynamics of Cylinder-Induced Shock-Wave/Transitional Boundary-Layer Interactions

Christopher S. Combs; E. Lara Lash; Phillip A. Kreth; John D. Schmisseur

2018 Fluid Dynamics Conference | 2018

Investigation of the Streamwise Development of Distributed Surface Roughness Effects on Supersonic Flows

Brian D. Kocher; Christopher S. Combs; Phillip A. Kreth; John D. Schmisseur

2018 AIAA Aerospace Sciences Meeting | 2018

The Role of Boundary-Layer Thickness on Cylinder-Generated Shock-Wave/Turbulent Boundary-Layer Interactions, Part I: Computations

Christopher S. Combs; Stefen A. Lindörfer; Phillip A. Kreth; John D. Schmisseur

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Christopher S. Combs

University of Tennessee Space Institute

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John D. Schmisseur

University of Tennessee

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E. Lara Lash

University of Tennessee Space Institute

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Stefen A. Lindörfer

University of Tennessee

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Brian D. Kocher

University of Tennessee

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Adam J. Harris

University of Tennessee

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Ryan B. Bond

University of Tennessee

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