# positions[].organizations[].parent[].label
Texas A&M Engineering Experiment Station (TEES)

# overview
Dr. Rodney Bowersox is the Department Head and Ford I Professor of Aerospace Engineering at Texas A&M University, College Station TX. He is the founder and director of the Texas A&M University National Aerothermochemistry and Hypersonics Laboratory. His research focus is on theoretical and experimental hypersonic viscous flows (turbulent and transitional), non-equilibrium gas dynamics, turbulence modeling, laser diagnostics, high-speed aerodynamics, sonic boom, and scramjet flows. He also develops state-of-the-art research facilities; for example, he designed two facilities for the AFRL air vehicle and directed energy directorates. He has received research sponsorship from the AFOSR, AFRL, ARO, DoD, NASA, NSF, ONR, and private industry. Dr. Bowersox is a DoD Vannevar Bush Faculty Fellow, a Fellow of the American Society of Mechanical Engineers, Associate Fellow of the American Institute of Aeronautics and Astronautics, and a member of the American Chemical Society, the American Physical Society, the Optical Society of America, and the International Society of Airbreathing Propulsion. He is an Associate Editor of the AIAA Journal of Propulsion and Power.

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4009 Electronics, Sensors And Digital Hardware

# keywords[]
5102 Atomic, Molecular And Optical Physics

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
0306 Physical Chemistry (incl. Structural)

# keywords[]
5102 Atomic, Molecular And Optical Physics

# keywords[]
5102 Atomic, Molecular And Optical Physics

# keywords[]
5102 Atomic, Molecular And Optical Physics

# 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
Virginia Tech - (Blacksburg, Virginia, United States)

# educationAndTraining[].organization.label
Virginia Tech - (Blacksburg, Virginia, United States)

# educationAndTraining[].organization.label
Virginia Tech - (Blacksburg, Virginia, United States)

# publications[].label
A two-color particle imaging velocimetry system for supersonic flow studies

# publications[].label
Comparison of measured and computed Strehl ratios for light propagated through a channel flow of a He-N(2) mixing layer at high Reynolds numbers.

# publications[].label
Freestream Disturbance Effects on Boundary Layer Instability and Transition on the AFOSR BOLT Geometry

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

# publications[].label
Minimization of sonic boom on supersonic aircraft using an evolutionary algorithm

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

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

# publications[].label
On the unsteady shock wave interaction with a splitter plate: Inviscid analysis

# publications[].label
Second-order reynolds stress turbulence modeling of three-dimensional oblique supersonic injection

# publications[].label
Digital analysis of shadowgraph images for statistical index of refraction (density) turbulent fluctuation properties in high-speed flow

# publications[].label
Influence of Perturbations on 3-D Hypersonic Shock Laminar Boundary Interactions

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

# publications[].label
Turbulent Flow Structure Characterization of Angled Injection into a Supersonic Crossflow

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

# publications[].label
Characterizing the Transient Growth Mechanism on a Hypersonic Blunt Body at a High Angle of Attack

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

# publications[].label
Experimental Investigation of Roughness Effects on Transition on Blunt Spherical Capsule Shapes

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

# publications[].label
Leading-Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil

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

# publications[].label
Application of Molecular Tagging Towards Simultaneous Vibrational Temperature and Velocity Mapping in an Underexpanded Jet Flowfield

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

# 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
Digital two-color PIV and flow-visualization studies for complex supersonic flows

# publications[].label
Supersonic Boundary-Layer Combustion: Effects of Upstream Entropy and Shear-Layer Thickness

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

# publications[].label
Compressible turbulence measurements in a supersonic boundary layer with impinging shock wave interaction

# publications[].label
Characterization of a Glow Discharge in a Tripped Hypersonic Boundary Layer

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

# publications[].label
Experimental investigation of low blow ratio blended missile body supersonic jet interaction flowfields

# publications[].label
Simultaneous velocity and temperature measurements in gaseous flow fields using the VENOM technique.

# publications[].label
Response of a supersonic turbulent boundary layer to periodic surface roughness

# publications[].label
Measurements of Turbulent Flow Structure in Supersonic Curved Wall Boundary Layers

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

# publications[].label
Supersonic missile body jet interaction flowfields at low momentum-parameter-ratio

# publications[].label
Algebraic turbulent energy flux models for hypersonic shear flows (vol 46, pg 49, 2010)

# publications[].label
Extension of equilibrium turbulent heat flux models to high-speed shear flows

# publications[].label
Optimizing scramjet fuel injection array design

# publications[].label
Skin friction gauges for high enthalpy impulsive flows

# publications[].label
A method to analyze molecular tagging velocimetry data using the Hough transform.

# publications[].label
Sonic boom alleviation using keel configurations

# publications[].label
Transverse injection through diamond and circular ports into a Mach 5.0 freestream

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

# publications[].label
Sonic injection into a Mach 5.0 freestream through diamond orifices

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

# publications[].label
Algebraic turbulent energy flux models for hypersonic shear flows: Invited presentation

# 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
Statistical assessment of optical phase fluctuations through turbulent mixing layers

# publications[].label
Sonic Boom Alleviation Using Keel Configurations

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

# publications[].label
Jet Interaction in Supersonic Flow with a Downstream Surface Ramp

# 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
Direct measurements of skin friction in complex supersonic flows

# publications[].label
Flowfield studies of a diamond-shaped fuel 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
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
Skin friction measurements in short duration high enthalpy flows

# publications[].label
Visualization of hypersonic turbulent boundary layers negotiating convex curvature

# publications[].label
Periodic surface roughness in high-speed turbulent flow

# publications[].label
Response of supersonic turbulent boundary layers to local and global mechanical distortions

# publications[].label
Examination of cameras for near-wall PIV measurements in high speed flows

# publications[].label
Non-statistical intermolecular energy transfer from vibrationally excited benzene in a mixed nitrogen-benzene bath.

# publications[].label
Tripping of a Hypersonic Low-Reynolds-Number Boundary Layer

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

# publications[].label
Experimental Investigation of the Flow Structure Near a Single Wraparound Fin

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

# publications[].label
Skin friction measurements in a Mach 6 inlet test

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

# publications[].label
Molecular Tagging Using Vibrationally Excited Nitric Oxide in an Underexpanded Jet Flowfield

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

# publications[].label
Simulation of transverse gaseous injection through a diamond port into a Mach 5.0 freestream

# publications[].label
Piv of a mach 5 turbulent boundary layer over diamond roughness elements

# publications[].label
Influence of surface roughness on the mean and turbulence flow properties of a supersonic boundary layer

# publications[].label
Towards Simultaneous Velocimetry and Thermometry Measurements Using the VENOM Diagnostic Technique

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

# publications[].label
Experimental investigation of supersonic gaseous injection into a supersonic freestream

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

# publications[].label
Jet Interaction in Supersonic Flow with a Downstream Surface Ramp

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

# publications[].label
Radiofrequency plasma stabilization of a low-Reynolds-number channel flow

# publications[].label
Asymptotic behaviour at the wall in compressible turbulent channels

# publications[].label
Digital two-color PIV measurements in a Mach-2.8 boundary layer

# publications[].label
Skin friction correlations for high enthalpy flows

# publications[].label
Two-Dimensional Nonadiabatic Injection into a Supersonic Freestream

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

# publications[].label
Two-component molecular tagging velocimetry utilizing NO fluorescence lifetime and NO2 photodissociation techniques in an underexpanded jet flowfield.

# publications[].label
Crosshatch roughness distortions on a hypersonic turbulent boundary layer

# publications[].label
Effect of transpiration cooling on nozzle heat transfer

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

# publications[].label
Experimental investigation of supersonic gaseous injection into a supersonic freestream

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

# publications[].label
Jet Interaction with a Primary Jet and an Array of Smaller Jets

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

# publications[].label
Transition due to Roughness on Blunt Capsule: Comparison with Transient Growth Correlation

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

# publications[].label
Vibrationally excited NO tagging by NO(A) fluorescence and quenching for simultaneous velocimetry and thermometry in gaseous flows.

# publications[].label
Numerical analysis of high-speed flow over rough surfaces

# publications[].label
Experimental Investigation of the Flow Structure Near a Single Wraparound Fin

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

# publications[].label
The role of near resonance electronic energy transfer on the collisional quenching of NO (A2+) by C6H6 and C6F6 at low temperature

# publications[].label
Flow Properties of a Supersonic Turbulent Boundary Layer with Wall Roughness

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

# publications[].label
Experimental investigation of the leading-edge flow of a dynamically pitching airfoil

# publications[].label
Measurements of compressible turbulent flow structure in a supersonic mixing layer

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

# publications[].label
Statistical anisotropy in free turbulence for mixing layers at high Reynolds numbers.

# publications[].label
Hypersonic Stability and Breakdown Measurements on the AFRL/AFOSR BOLT II Flight Geometry

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

# publications[].label
Freestream Effects on Boundary Layer Disturbances for HIFiRE-5

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

# publications[].label
Gaseous injection through diamond orifices at various incidence angles into a hypersonic freestream

# publications[].label
Numerical analyses of gaseous injection into a mach 5.0 freestream through diamond orifices

# publications[].label
Sonic injection into a mach 5.0 freestream through diamond orifices at various incidence

# publications[].label
On the design and construction of an academic mach 5 wind tunnel

# publications[].label
Effect of a normal shock wave on freestream total pressure fluctuations in a low-density mach 6 flow

# publications[].label
Numerical Investigation of Supersonic Injection Using a Reynolds-Stress Turbulence Model

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

# publications[].label
Planar measurements of supersonic boundary layers with curvature driven pressure gradients

# publications[].label
Supersonic Boundary Layers with Periodic Surface Roughness

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

# publications[].label
Experimental Analysis of the Turbulent Shear Stresses for Distorted Supersonic Boundary Layers

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

# publications[].label
The Mach 6 Quiet Tunnel at Texas A&M: Quiet flow performance

# publications[].label
Mass-weighted turbulence measurements in a Mach 2.9 boundary layer with mild adverse and favorable pressure gradient

# publications[].label
Combined laser Doppler velocimetry and cross-wire anemometry analysis for supersonic turbulent flow

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

# publications[].label
Survey of high-speed rough wall boundary layers: Invited presentation

# publications[].label
The Effect of Vibrational Non-Equilibrium on the Decay of Grid Generated Turbulence

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

# publications[].label
The effect of diamond injector geometry on supersonic jet interaction secondary flow

# publications[].label
Effects of Mach Number on Supersonic Wraparound Fin Aerodynamics

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

# publications[].label
Aerodynamics of Low-Blowing-Ratio Fuselage Injection into a Supersonic Freestream

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

# publications[].label
Jet Interaction with a Main Jet and an Array of Smaller Jets: Part A - Experimental Studies

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

# publications[].label
Simultaneous three-dimensional velocimetry and thermometry in gaseous flows using the stereoscopic vibrationally excited nitric oxide monitoring technique.

# publications[].label
Experimental Analysis of the Turbulent Shear Stresses for Distorted Supersonic Boundary Layers

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

# publications[].label
Studies of diamond-shaped injectors in a supersonic flow

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

# publications[].label
Transpiration cooling effects on nozzle heat transfer and performance

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

# publications[].label
Performance characterization of a highly offset diffuser with vortex generator jets

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

# publications[].label
The role of downstream ramps on penetration and mixing enhancement for supersonic injection flows

# publications[].label
Internal energy based modeling of high-speed gaseous flow turbulence

# publications[].label
Jet Interaction with a Main Jet and an Array of Smaller Jets: Part A - Experimental Studies

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

# publications[].label
Heat transfer and skin friction in a Mach 6: Inlet flow

# publications[].label
Hypersonic Boundary Layer Cross Flow Transition - Characteristics and Control

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

# publications[].label
Freestream Turbulence Measurements in a Continuously Variable Hypersonic Wind Tunnel

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

# publications[].label
Repetitively Pulsed Hypersonic Test Facility for Advanced Laser Diagnostic Development

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

# publications[].label
Velocity and temperature fluctuations in a high-speed shock-turbulence interaction

# publications[].label
On the unsteady shock wave interaction with a backward-facing step: Inviscid analysis

# publications[].label
Turbulence measurements in a Mach 2.9 boundary layer including mild pressure gradients

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

# publications[].label
Experimental Investigation of the Role of Downstream Ramps on a Supersonic Injection Plume

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

# publications[].label
Characterization of the flowfield near a wrap-around fin at Mach 2.8

# 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
Characterization of the three dimensional turbulent flow structure of angled injection into a supersonic cross flow

# publications[].label
Compressible turbulence measurements in supersonic boundary layers with favorable and adverse pressure gradients

# publications[].label
Measurements of Natural Transition During the BOLT II Flight Experiment

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

# publications[].label
Algebraic turbulent energy flux models for hypersonic shear flows

# publications[].label
Repetitively Pulsed Hypersonic Flow Apparatus for Diagnostic Development

# 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
Influence of Curvature-Driven Favorable Pressure Gradient on Supersonic Turbulent Boundary Layer

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

# publications[].label
Turbulence and meanflow measurements downstream of a two-dimensional supersonic normal injection into a supersonic freestream

# publications[].label
Jet Interaction in Supersonic Flow with a Surface Ramp

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

# publications[].label
Structure of a compressible boundary layer over a curved wall

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

# publications[].label
Resolving the energy and temperature dependence of C6H6 () collisional relaxation via time-dependent bath temperature measurements.

# publications[].label
The characterization and feasibility of a low-duty-cycle fast valve for impulse facilities

# publications[].label
Flow structure and performance characterization of an offset diffuser with and without vortex generator jets

# publications[].label
Two-Component Molecular Tagging Velocimetry Utilizing NO Fluorescence Lifetime and NO2 Photodissociation Techniques in an Underexpanded Jet Flowfield

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

# publications[].label
Experimental Investigations of Roughness Effects on Transition on Blunt Spherical Capsule Shapes

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

# publications[].label
Characterization of flow structures and turbulence in hypersonic jet interaction flowfields

# publications[].label
Gas flow visualization by means of sheared beam interferometry: sensitivity, maximum measurable gradient of the density fluctuation, and integrated density estimation

# publications[].label
Visualization of the structural response of a hypersonic turbulent boundary layer to convex curvature

# publications[].label
Examination of the leading edge flow structure of a dynamically pitching NACA 0012 airfoil

# publications[].label
Compressible turbulence measurements in a high-speed high-Reynolds-number mixing layer

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

# publications[].label
Flow properties of compressible and incompressible subsonic turbulent boundary layers with surface roughness

# publications[].label
Experimental investigation of supersonic wrap-around fin aerodynamic Mach number effects

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

# 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)

# publications[].label
Flow field studies of diamond shaped fuel injector in a supersonic flow

# publications[].label
Role of the barrel shock as control element for hypersonic transverse jet injection flows

# publications[].label
Temporal Turbulent Flow Structure for Supersonic Rough-Wall Boundary Layers

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

# publications[].label
Simulation of transverse gaseous injection through diamond ports into supersonic freestream

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

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

# publications[].label
Technique for direct measurement of skin friction in high enthalpy impulsive scramjet flowfields

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

# publications[].label
Leading-Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil

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

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

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

# publications[].label
Characterization of the flow structure in the vicinity of a wrap-around fin at supersonic speeds

# publications[].label
Low-temperature collisional quenching of NO A(2)(+)(v' = 0) by NO(X(2)) and O2 between 34 and 109 K.

# publications[].label
Model for compressible turbulence in hypersonic wall boundary and high-speed mixing layers

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

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

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

# publications[].label
Temperature perturbation related to the invisible ink vibrationally excited nitric oxide monitoring (VENOM) technique: a simulation study.

# publications[].label
High-Speed Free Shear Layers with Molecular Non-Equilibrium: An Example of the Fluids Information Triad (Invited)

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

# publications[].label
The influence of favorable pressure gradients upon the coherent motions in a Mach 5 turbulent boundary layer

# publications[].label
Characterization of the flowfield near a wrap-around fin at mach 4.9

# publications[].label
Minimization of sonic boom on supersonic aircraft using an evolutionary algorithm

# publications[].label
Simultaneous velocity and temperature measurements in gaseous flowfields using the vibrationally excited nitric oxide monitoring technique: a comprehensive study.

# publications[].label
High-speed planar laser-induced fluorescence investigation of nitric oxide generated by hypersonic Mach reflections for computational fluid dynamics validation

# researcherOn[].label
2013-2014 Aeronautics Scholarship Program (Student Name:  Alejandro Azocar)

# researcherOn[].awardedBy.label
National Aeronautics and Space Administration - (Washington D.C., District of Columbia, United States)

# researcherOn[].awardedBy.label
United States Army - (Washington D.C., District of Columbia, United States)

# researcherOn[].label
(DURIP-17) INSTRUMENTED HYPERVELOCITY RESEARCH TUNNEL NOZZLE

# researcherOn[].awardedBy.label
United States Air Force - (Arlington, Virginia, United States)

# researcherOn[].awardedBy.preferredLabel
DOD-Air Force-Office of Scientific Research

# researcherOn[].label
One Stop Shopping Initiative - NASA Scholarship (MUREP) - 2013 MUREP Scholarship (Student:  Alexxandra Cisotto)

# researcherOn[].awardedBy.label
National Aeronautics and Space Administration - (Washington D.C., District of Columbia, United States)

# researcherOn[].label
USAFA: Hypersonic Turbulent Wall Heat Transfer Prediction and Validation

# researcherOn[].awardedBy.label
United States Air Force - (Arlington, Virginia, United States)

# researcherOn[].awardedBy.label
United States Air Force - (Arlington, Virginia, United States)

# researcherOn[].label
ARL: Innovative Ecosystem Performance Research

# researcherOn[].awardedBy.label
United States Army - (Washington D.C., District of Columbia, United States)

# researcherOn[].label
Turbulence Control Through Thermal Non-Equilibrium: Molecular Relaxation Models and Implications for Turbulence Modeling

# researcherOn[].awardedBy.label
United States Air Force - (Arlington, Virginia, United States)

# researcherOn[].awardedBy.preferredLabel
DOD-Air Force-Office of Scientific Research

# researcherOn[].label
Hypervelocity Expansion Facility for Fundamental High-Enthalpy Research

# researcherOn[].awardedBy.label
United States Department of the Navy - (Arlington, Virginia, United States)

# researcherOn[].label
Hypersonic Boundary Layer Turbulance (BOLT-II) Flight Test Experiment

# researcherOn[].awardedBy.label
United States Air Force - (Arlington, Virginia, United States)

# researcherOn[].awardedBy.preferredLabel
DOD-Air Force-Office of Scientific Research

# researcherOn[].label
IUSE/PFE: RED: REvolutionizing Diversity Of Engineering (REDO-E)

# researcherOn[].awardedBy.label
National Science Foundation - (Arlington, Virginia, United States)

# researcherOn[].label
FFATA: REU: AERO-U: Aerospace Engineering Research Opportunities for Undergraduates

# researcherOn[].awardedBy.label
National Science Foundation - (Arlington, Virginia, United States)

# researcherOn[].label
Hypersonic Turbulent Wall Heat Transfer Prediction and Validation - ONR Simulations

# researcherOn[].awardedBy.label
United States Department of the Navy - (Arlington, Virginia, United States)

# researcherOn[].awardedBy.label
National Aeronautics and Space Administration - (Washington D.C., District of Columbia, United States)

# researcherOn[].label
Crossflow Instability Receptivity to Environmental Disturbances at Hypersonic Speeds

# researcherOn[].awardedBy.label
United States Air Force - (Arlington, Virginia, United States)

# researcherOn[].awardedBy.preferredLabel
DOD-Air Force-Office of Scientific Research

# researcherOn[].label
Turbulence Transport in Extreme Non-Equilibrium Environments

# researcherOn[].awardedBy.label
United States Department of the Navy - (Arlington, Virginia, United States)

# researcherOn[].label
Boundary Layer Transition (BOLT) - Experiment and Simulation (Concave Curvature and Leading Edge Sweep Effects)

# researcherOn[].awardedBy.label
United States Air Force - (Arlington, Virginia, United States)

# researcherOn[].awardedBy.preferredLabel
DOD-Air Force-Office of Scientific Research

# researcherOn[].label
Thermal and Mechanical Non-Equilibrium Effects on Turbulent Flows: Fundamental Studies of Energy Exchanges through Direct Numerical Simulations, Molecular Simulations and Experiments

# researcherOn[].awardedBy.label
United States Air Force - (Arlington, Virginia, United States)

# researcherOn[].awardedBy.preferredLabel
DOD-Air Force-Office of Scientific Research

# streetAddress
Texas A&M University; Aerospace Engineering; 3141 TAMU

# organizations[]
Texas A&M Engineering Experiment Station (TEES)

# schools[]
Texas A&M Engineering Experiment Station (TEES)

# inTheNews[].label
DOD Awards Applied Hypersonics Contract to Texas A&M University

# inTheNews[].label
Texas A&M System To Lead $100 Million Hypersonic Research Consortium

# inTheNews[].label
Texas A&M to lead $100M hypersonic research project

# etdChairOf[].label
English, Benjamin L. (2013-04). Large-Scale Streamwise Turbulent Structures in Hypersonic Boundary Layers. Master's Thesis.

# etdChairOf[].label
McLellan, Justin Walter (2006-10). The effects of diamond injector angles on flow structures at various Mach numbers. Master's Thesis.

# etdChairOf[].label
Kostak, Heather Emily (2020-03). Ground Test Analyses of the AFOSR Boundary Layer Transition (BOLT) Flight Geometry. Master's Thesis.

# etdChairOf[].label
Mendoza, Nicole Renee (2013-04). On the Fundamental Unsteady Fluid Dynamics of Shock-Induced Flows through Ducts. Doctoral Dissertation.

# etdChairOf[].label
Peltier, Scott Jacob (2013-08). Behavior of Turbulent Structures within a Mach 5 Mechanically Distorted Boundary Layer. Doctoral Dissertation.

# etdChairOf[].label
Tichenor, Nathan Ryan (2009-05). Particle image velocimetry in an advanced, serpentine jet engine inlet duct. Master's Thesis.

# etdChairOf[].label
Sahoo, Dipankar (2008-10). Experimental analysis of the vorticity and turbulent flow dynamics of a pitching airfoil at realistic flight (helicopter) conditions. Doctoral Dissertation.

# etdChairOf[].label
Leidy, Andrew Norbert (2019-01). An Experimental Characterization of 3-D Transitional Shock Wave Boundary Layer Interactions at Mach 6. Doctoral Dissertation.

# etdChairOf[].label
Mai, Chi Luong Nhat (2014-05). Near-Region Modification of Total Pressure Fluctuations by a Normal Shock Wave in a Low-Density Hypersonic Wind Tunnel. Doctoral Dissertation.

# etdChairOf[].label
Srinivasan, Ravichandra (2006-04). Improved understanding and control of high-speed jet interaction flows. Doctoral Dissertation.