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

    Combs, Christopher S. / Lash, E. Lara / Kreth, Phillip A. et al. | AIAA | 2018

    Unsteady Analysis of Shock-Wave/Boundary-Layer Interaction Experiments at Mach 4.2

    Combs, Christopher S. / Schmisseur, John D. / Bathel, Brett F. et al. | AIAA | 2019

    Application of Pressure-Sensitive Paint to Investigate Hypersonic Shock-Wave/ Boundary-Layer Interactions

    Andrade, Angelina / LaLonde, Elijah J. / Hoffman, Eugene N. et al. | AIAA | 2023

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

    Lash, E. Lara / Combs, Christopher S. / Kreth, Phillip A. et al. | AIAA | 2016

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

    Combs, Christopher S. / Kreth, Phillip A. / Schmisseur, John D. et al. | AIAA | 2017

    Heat-Shield Ablation Visualized Using Naphthalene Planar Laser-Induced Fluorescence

    Combs, Christopher S. / Clemens, Noel T. / Danehy, Paul M. et al. | AIAA | 2017

    Effects of distributed roughness on shock-wave/boundary-layer interactions at Mach 7.2

    Hoffman, Eugene N. / Kendhammer, David M. / LaLonde, Elijah J. et al. | AIAA | 2023

    Investigation of the Effects of Distributed Surface Roughness on Supersonic Flows

    Kocher, Brian D. / Combs, Christopher S. / Kreth, Phillip A. et al. | AIAA | 2017

    An Investigation of the Role of an Upstream Burst Diaphragm on Flow Quality within a Ludwieg Tube using RANS

    Lindörfer, Stefen A. / Anusonti-Inthra, Phuriwat / Combs, Christopher S. et al. | AIAA | 2016

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

    Lindörfer, Stefen A. / Combs, Christopher S. / Kreth, Phillip A. et al. | AIAA | 2017

    Characterizing Streamwise Development of Surface Roughness Effects on a Supersonic Boundary Layer

    Kocher, Brian D. / Kreth, Phillip A. / Schmisseur, John D. et al. | AIAA | 2022

    Modal Analysis of a Sweeping Jet Emitted by a Fluidic Oscillator

    Portillo, Daniel J. / Hoffman, Eugene N. / Garcia, Matt et al. | AIAA | 2021

    High-Speed Pressure Sensitive Paint Measurements of the Initial Concept 3.X Vehicle at Mach 7

    Dhanagopal, Abinayaa / Williamson, Chad / LaLonde, Elijah J. et al. | AIAA | 2023

    Preliminary Testing of the UTSA Mach 7 Ludwieg Tube

    Hoffman, Eugene N. / Rodriguez, Jose M. / Garcia, Matt et al. | AIAA | 2021

    Characterization of the UTSA Mach 7 Ludwieg Tube

    Hoffman, Eugene N. / LaLonde, Elijah J. / Garcia, Matt et al. | AIAA | 2022

    Flow Control of Hypersonic Shock-Wave/Boundary-Layer Interactions Using Phononic Metamaterials

    Navarro, Juan D. / Velasquez, Juan Camilo C. / LaLonde, Elijah J. et al. | AIAA | 2024

    Development of MIR TLAS System with Applications to Reacting Hot Gas Flows

    Sweetland, Katrina / Combs, Christopher S. / Schmisseur, John D. et al. | AIAA | 2018

    High-speed laser absorption measurements of temperature and carbon oxides in linear detonation channels

    Fetter, Kyle L. / Steavenson, Benjamin / Donald, Brandon et al. | AIAA | 2023

    Shockwave/Boundary-Layer Interaction Studies Performed in the NASA Langley 20-Inch Mach 6 Air Tunnel

    Bathel, Brett F. / Jones, Stephen B. / Watkins, Neal et al. | AIAA | 2019

      Shockwave/Boundary-Layer Interaction Studies Performed in the NASA Langley 20-Inch Mach 6 Air Tunnel

      Bathel, Brett F. / Jones, Stephen B. / Watkins, Anthony N. et al. | AIAA | 2019