# positions[].organizations[].label
George H.W. Bush Combat Development Complex

# positions[].organizations[].label
George H.W. Bush Combat Development Complex

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4007 Control Engineering, Mechatronics And Robotics

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# educationAndTraining[].organization.label
Texas A&M University - (College Station, Texas, United States)

# educationAndTraining[].organization.label
Texas A&M University - (College Station, Texas, United States)

# educationAndTraining[].organization.label
Texas A&M University - (College Station, Texas, United States)

# publications[].label
Reynolds Stresses in a Hypersonic Boundary Layer with Streamline Curvature-Driven Favorable Pressure Gradients

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Hypervelocity Research Tunnel for Fundamental High-Enthalpy Research

# publications[].label
Proper Orthogonal Decomposition Analysis of Hypersonic Turbulent Boundary Layers Subjected to Streamline Wall Curvature

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Some effects of tunnel noise on cylinder-induced Mach 6 transitional shock wave boundary layer interactions

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Cycloidal Rotor-Blade Tip-Vortex Analysis at Low Reynolds Number

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Towards Supersonic Flat-Wall Flame Holding with Nanosecond-Pulsed High-Frequency Discharges

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Hypersonic Boundary Layer Transition Measurements using Wall Shear Sensors

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
High-Speed Schlieren Imaging and Hot-wire Characterization of Cylinder-Induced Hypersonic Shock Boundary Layer Interactions

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Characterization of the influence of a favorable pressure gradient on the basic structure of a Mach 5.0 high Reynolds number supersonic turbulent boundary layer

# publications[].label
Instantaneous Wind-Tunnel Model Vibration Measurements Using a Kalman Filtering Approach

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
On the Design and Calibration of an Actively Controlled Expansion Hypersonic Wind Tunnel

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
The Effects of Laser Plasma Discharge on a Separating Boundary Layer

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Experimental Investigation of Laser-Based Flow Modification Over a Low Speed Airfoil

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Hypersonic Boundary Layer with Streamline Curvature-Driven Adverse Pressure Gradient

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Numerical Simulation of Supersonic Turbulent Boundary Layers Subjected to Favorable Pressure Gradients

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Influence of Favorable Pressure Gradients on a Mach 5.0 Turbulent Boundary Layer

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Boundary-Layer Separation Control Using Laser-Induced Air Breakdown

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Particle image velocimetry in an advanced, serpentine jet engine inlet duct

# publications[].label
Active control of jet engine inlet flows

# publications[].label
Turbulent / Non-Turbulent Interface and Uniform Momentum Zones of High-Speed Turbulent Boundary Layers Subjected to Streamline Pressure Gradient

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Cylinder-Induced Hypersonic Transitional Shock Wave Boundary Layer Interactions: Pressure Fluctuations and Thermal Loading

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Fluid-Structure Interaction Modeling of a Shape-Memory Alloy Actuated Supersonic Wind Tunnel Model Alloy

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Tip vortex measurements on a cycloidal rotor blade at ultralow Reynolds numbers

# publications[].label
Thermal transport in hypersonic turbulent boundary layers at high-Reynolds numbers

# publications[].label
Investigation of Partially-Coupled Ignition Using Nanosecond Pulsed High Frequency Discharges

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Experimental and numerical studies of diamond-shaped injector in a supersonic flow

# publications[].label
Boundary-layer separation control using laser-induced air breakdown

# publications[].publisher
American Institute of Aeronautics and Astronautics

# publications[].label
Effects of Fuel Mixture Properties on Nanosecond Pulsed High Frequency Discharge Ignition

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Experimental and Numerical Studies of Diamond-Shaped Injector in a Supersonic Flow

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Experimental and Numerical Studies of Diamond-Shaped Injector in a Supersonic Flow

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Influence of Environmental Disturbances on Hypersonic Crossflow Instability on the HIFiRE-5 Elliptic Cone

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Response of a hypersonic turbulent boundary layer to favourable pressure gradients

# publications[].label
Calibration of an Actively Controlled Expansion Hypersonic Wind Tunnel

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Influence of Streamline Adverse Pressure Gradients on the Structure of a Mach 5 Turbulent Boundary Layer

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Characterization of Environmental Disturbances on Hypersonic Crossflow Instability on the HIFiRE-5 Elliptic Cone

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# streetAddress
Texas A&M Engineering Experiment Station; Aerospace Engineering; 3141 TAMUS

# organizations[]
George H.W. Bush Combat Development Complex

# etdChairOf[].label
Carlson, Joseph Douglas (2022-12). Curvature-Driven Favorable Pressure Gradient Effects on Shock Boundary Layer Interactions. Doctoral Dissertation.