# positions[].organizations[].label
Institute for Engineering Education and Innovation

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

# 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

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# educationAndTraining[].organization.label
California Institute of Technology - (Pasadena, California, United States)

# publications[].label
Preliminary Results on the Effect of Phase Angle on Coaxial Jet Behavior spanning Sub- to Supercritical Pressures

# publications[].label
Development of the Scorpius LOX/Kerosene Engine Family

# publications[].label
Shock detachment process in hypervelocity flow over a cone

# publications[].label
The seismic response of an aquifer to the propagation of an impact generated shock wave: A possible trigger of the Martian outflow channels

# publications[].label
Receptivity of a Cryogenic Coaxial Gas-Liquid Jet to Acoustic Disturbances

# publications[].label
Shock Tunnel Operation and Correlation of Boundary Layer Transition on a Cone in Hypervelocity Flow

# publications[].label
Aircraft and detonative engine incorporating pulse detonation engines

# publications[].label
Development of a Facility for Combustion Stability Experiments at Supercritical Pressure

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

# publications[].label
Transition Within a Hypervelocity Boundary Layer on a 5-Degree Half-Angle Cone in Air/CO2 Mixtures

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

# publications[].label
On the Effect of a Transverse Acoustic Field on a Flush Shear Coaxial Injector

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

# publications[].label
Effects of Shock-Tube Cleanliness on Slender-Body Hypersonic Instability and Transition Studies at High-Enthalpy

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

# publications[].label
Preliminary Results on Coaxial Jet Sprean Angles and the Effects of Variable Phase Transverse Acoustic Fields

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

# publications[].label
Effect of Variable Phase Transverse Acoustic Fields on Coaxial Jet Forced Spread Angles

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

# publications[].label
Receptivity of a Cryogenic Coaxial Gas-Liquid Jet to Acoustic Disturbances

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

# publications[].label
Laser-induced thermal acoustics (LITA) signals from finite beams.

# publications[].label
Transition Delay in Hypervelocity Boundary Layers by Means of CO2/Acoustic Instability Interactions

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

# publications[].label
Introduction to the Virtual Collection on the Boundary Layer Turbulence Flight Experiment in Memory of Mike Holden (BOLT II)

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

# publications[].label
Fuel preconditioning for detonation combustion

# publications[].label
Pulse detonation system for a gas turbine engine

# publications[].label
A Constrained Space Exploration Technology Program A Review of NASA's Exploration Technology Development Program

# publications[].label
Numerical Study of the Origin of Heat Streaks on a Second-Order Continuous, Swept Geometry in Hypersonic Flow

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

# publications[].label
A Review of United States Air Force and Department of Defense Aerospace Propulsion Needs

# publications[].label
Unsteady Disturbance Amplification on a Wedge at Mach 6

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

# publications[].label
Numerical Simulations of Direct Initiation of Detonations in Hydrocarbon Fuel/air Mixtures

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

# publications[].label
Geometry Effects on Steady and Acoustically Forced Shear-Coaxial Jet Sprays

# publications[].label
Experimental and Computational Study of High Enthalpy Double-Wedge Flows

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

# publications[].label
Split Stream Flow Past a Blunt Trailing Edge with Application to Combustion Instabilities

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

# publications[].label
Forced and Unforced Shear Coaxial Mixing and Combustion at Subcritical and Supercritical Pressures

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

# publications[].label
Shock Tunnel Operation and Correlation of Boundary Layer Transition on a Cone in Hypervelocity Flow

# publications[].label
Mixing Enhancement of Liquid Rocket Engine Injector Flow

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

# publications[].label
Results of Subcritical One-Phase Coaxial Jet Spread Angles and Subcritical to Supercritical Acousticall-Forced Coaxial Jet Dark Core Lengths

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

# publications[].label
Introduction to the Special Section on the Boundary Layer Transition (BOLT) Flight Experiment

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

# publications[].label
An Experimental Investigation on the Origin of Heat Streaks for Swept Geometries in Hypersonic Flows

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

# publications[].label
Mixing under Transcritical Coaxial Injection Conditions: Experiments and Simulations

# publications[].label
Effects of a Variable-Phase Transverse Acoustic Field on a Coaxial Injector at Subcritical and Near-Critical Conditions

# publications[].label
MEMS-based pulse detonation engine for small-scale propulsion applications

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

# publications[].label
MEMS-based pulse detonation engine for small scale propulsion applications

# publications[].label
Shock wave reflector and detonation chamber

# publications[].label
A Numerical Investigation on the Origin Mechanisms for Heat Streaks on Swept Geometries in Hypersonic Flows

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

# publications[].label
Transition Delay in a Hypervelocity Boundary Layer using Nonequilibrium CO2 Injection

# publications[].label
Computational Fluid Dynamics Analysis of the Infrared Emission From a Generic Hypersonic Glide Vehicle

# publications[].label
Turbulent Spot Observations within a Hypervelocity Boundary Layer on a 5-degree Half-Angle Cone

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

# publications[].label
Transition Within a Hypervelocity Boundary Layer on a 5-Degree Half-Angle Cone in Air/CO2 Mixtures

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

# publications[].label
The Response of Cryogenic H2/O2 Coaxial Jet Flames to Acoustic Disturbances

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

# publications[].label
Cryogenic High-Pressure Shear-Coaxial Jets Exposed to Transverse Acoustic Forcing

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

# publications[].label
On the impact of injection schemes on transition in hypersonic boundary layers

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

# publications[].label
Effect of Gas Injection on Transition in Hypervelocity Boundary Layers

# publications[].label
Investigation of Unsteady Flow Field in a 2-Stage PDE Resonator

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

# publications[].label
Sonic Line and Shock Detachment in Hypervelocity Cone Flow

# publications[].label
Nano-ignition Torch Applied to Cryogenic H2/O2 Coaxial Jet

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

# publications[].label
Method and apparatus for modulating airfoil lift

# publications[].label
NASA Space Technology Roadmaps and Priorities Restoring NASA's Technological Edge and Paving the Way for a New Era in Space

# publications[].label
Decadal Survey of Civil Aeronautics Foundation for the Future

# publications[].label
An Experimental Investigation on the Origin of Heat Streaks for Swept Geometries in Hypersonic Flows

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

# publications[].label
Experiments and numerical simulation of mixing under supercritical conditions

# publications[].label
Proper Orthogonal Decomposition Analysis of Shear-Coaxial Injector Flows with and Without Transverse Acoustic Forcing

# publications[].label
Study of the addition of a divergent nozzle to an expansion tube for increasing test time

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

# publications[].label
Dark Core Analysis of Coaxial Injectors at Sub-, Near-, and Supercritical Conditions in a Transverse Acoustic Field

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

# publications[].label
Stability analysis of high-speed boundary-layer flow with gas injection

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

# publications[].label
Quantitative Analysis of Forced and Unforced Turbulent Multiphase Coaxial Jets

# publications[].label
The relentless pursuit of hypersonic flight

# publications[].label
Carbon Dioxide Injection for Hypervelocity Boundary Layer Stability

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

# publications[].label
Effects of Shock-Tube Cleanliness on Hypersonic Boundary Layer Transition at High Enthalpy

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

# organizations[]
Institute for Engineering Education and Innovation

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

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

# inTheNews[].label
Decoding the boundary layer at hypersonic speeds