# 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

# 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

# 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

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# educationAndTraining[].organization.label
University of New Mexico - (Valencia, New Mexico, United States)

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

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

# publications[].label
GENERATION OF CROSSFLOW VORTICES IN A THREE-DIMENSIONAL FLAT-PLATE FLOW.

# publications[].label
Crossflow instability on a yawed cone at Mach 6

# publications[].label
Flight experiments on swept wing transition using distributed roughness

# publications[].label
Experiments on the subharmonic route to turbulence in boundary layers.

# publications[].label
Experiments on the stability of nonlinear waves in a boundary layer.

# publications[].label
Computational Evaluation and Linear Stability of a Transonic Laminar-Flow Wing Glove

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

# publications[].label
Generation of crossflow vortices in a three-dimensional flat-plate flow.

# publications[].label
The Development of Crossflow Vortices on a 45 Degree Swept Wing

# publications[].label
On the deviatoric normal stress on a slip surface

# publications[].label
Influence of high-amplitude noise on boundary-layer transition to turbulence

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

# publications[].label
Flexible Flight Research Platform at Texas A&M University Flight Research Laboratory

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

# publications[].label
Passive control of transition in three-dimensional boundary layers, with emphasis on discrete roughness elements.

# publications[].label
Nonlinear stability of a liquid film adjacent to a supersonic stream

# publications[].label
Computational Investigation of the Effects of Surface Imperfections and Excrescences on the Crossflow Instability

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

# publications[].label
WAVELENGTH SELECTION AND TOTAL GROWTH OF GORTLER VORTICES.

# publications[].label
Non-linear acoustic response of a spherical bubble

# publications[].label
CFD Validation Issues for Boundary-Layer Stability and Transition

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

# publications[].label
Development of stationary crossflow vortices on a swept wing

# publications[].label
Effects of curvature variations on the nonlinear evolution of Goertler vortices

# publications[].label
Boundary-Layer Transition on a Flared Cone in the Texas A&M Mach 6 Quiet Tunnel

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

# publications[].label
CFD Analysis of Flight-Test Configuration for LFC on Swept Wings

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

# publications[].label
Roughness receptivity studies in a 3-D boundary layer - Flight tests and computations

# publications[].label
Mode competition in modulated Taylor-Couette flow

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

# publications[].label
Design of the Subsonic Aircraft Roughness Glove Experiment (SARGE)

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

# publications[].label
Laminar Flow Control on a Swept Wing with Distributed Roughness

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

# publications[].label
Stability and control of high-speed flows

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

# publications[].label
Design of Experiments with an Application to Laminar Flow Control Flight Research

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

# publications[].label
Incompressible Magnetohydrodynamic Entrance Flow in a Plane Channel

# publications[].label
NONLINEAR ACOUSTIC RESPONSE OF A SPHERICAL BUBBLE

# publications[].label
Flight experiments on the effects of step excrescences on swept-wing transition

# publications[].label
Flow quality issues for large wind tunnels

# publications[].label
Characterization of the flowfield structure of an annular dielectric barrier discharge plasma actuator

# publications[].label
Receptivity Measurements on a Swept-Wing Model

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

# publications[].label
Stability of liquid films adjacent to compressible streams

# publications[].label
EXPERIMENTS ON THE SUBHARMONIC ROUTE TO TURBULENCE IN BOUNDARY LAYERS.

# publications[].label
Crossflow-vortex instability and transition on a 45-degree swept wing

# publications[].label
Nonlinear wave interactions in supersonic wind-generated waves

# publications[].label
Crossflow instability in a hypersonic boundary layer

# publications[].label
Effects of step excrescences on a swept wing in a low-disturbance wind tunnel

# publications[].label
A Transonic Laminar-Flow Wing Glove Flight Experiment: Computational Evaluation and Linear Stability

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

# publications[].label
Direct Numerical Simulation of Discrete Roughness on a Swept-Wing Leading Edge

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

# publications[].label
Drag Reduction Initial Conditions on Various Legacy Fleet Aircraft: Surface Roughness Measurements

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

# publications[].label
Wavelength selection and growth of Goertler vortices

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

# publications[].label
Supersonic laminar flow control on swept wings using distributed roughness

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

# publications[].label
Boundary-layer transition to turbulence: the last five years.

# publications[].label
Experiments on the stability of the flat-plate boundary layer with suction

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

# publications[].label
Computational design of a test article to investigate 2-D surface excrescences on a swept laminar-flow wing

# publications[].label
Investigation of a health monitoring methodology for future natural laminar flow transport aircraft

# publications[].label
Receptivity: The Inspiration of Mark Morkovin (Invited)

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

# publications[].label
Laminar Flow Control on a Swept Wing with Distributed Roughness

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

# publications[].label
STABILITY AND TRANSITION OF THREE-DIMENSIONAL FLOWS.

# publications[].label
Transition Mechanisms for Transport Aircraft

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

# publications[].label
In-Flight Receptivity Experiments on a 30-degree Swept-Wing Using Micron-sized Discrete Roughness Elements

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

# publications[].label
Review of flow quality issues in wind tunnel testing

# publications[].label
Comparing local and marching analyses of Goertler instability

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

# publications[].label
Application of variable leading-edge roughness for transition control on swept wings

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

# publications[].label
Experiments on the stability of liquid films adjacent to supersonic boundary layers

# publications[].label
Effect of suction and weak mass injection on boundary-layer transition

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

# publications[].label
Crossflow Instabilities - Theory & Technology

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

# publications[].label
Flexible Flight Research Platform at Texas A&M University Flight Research Laboratory

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

# publications[].label
Boundary Layer Receptivity to Sound: Navier-Stokes Computations

# publications[].label
Complete Computational Fluid Dynamics Analysis of Velocity XL with Flight-Test Verification

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

# publications[].label
Flow Quality Measurements in the Klebanoff-Saric Wind Tunnel

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

# publications[].label
Stability, transition, and control of three-dimensional boundary layers on swept wings

# publications[].label
Effect of Isolated Micron-Sized Roughness on Transition in Swept-Wing Flows

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

# publications[].label
Control of Transition in Supersonic Boundary Layers: Experiments and Computations (Keynote)

# publications[].label
Effects of Step Excrescences on a Swept Wing in a Low-Disturbance Wind Tunnel

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

# publications[].label
WAVELENGTH SELECTION AND TOTAL GROWTH OF GORTLER VORTICES.

# publications[].label
STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS

# publications[].label
CFD validation issues in transition modeling

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

# publications[].label
Stability of Gortler Vortices in Boundary Layers

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

# publications[].label
Boundary-layer receptivity of three-dimensional roughness arrays on a swept-wing

# publications[].label
Gortler vortices with periodic curvature

# publications[].label
CFD Analysis of Flight-Test Configuration for LFC on Swept Wings

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

# publications[].label
Experiments on the stability of nonlinear waves in a boundary layer.

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

# publications[].label
Measurement of crossflow vortices, attachment-line flow, and transition using microthin hot films

# publications[].label
Boundary-layer instability and transition on a flared cone in a Mach 6 quiet wind tunnel

# publications[].label
An Experimental Investigation of the Stability of a Thin Liquid Layer Adjacent to a Supersonic Stream

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

# publications[].label
Nonlinear behaviour of the Mack mode in a hypersonic boundary layer

# publications[].label
Direct Numerical Simulation of Distributed Roughness on a Swept Wing Leading Edge

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

# publications[].label
Effects of Step Excrescences on Swept-Wing Transition

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

# publications[].label
Design of the Subsonic Aircraft Roughness Glove Experiment (SARGE)

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

# publications[].label
Laminar flow control on a swept Wing with distributed roughnesssss

# publications[].label
Generation of long subharmonic internal waves by surface waves

# publications[].label
Gortler vortices with periodic curvature

# publications[].label
Toward Practical Laminar Flow Control - Remaining Challenges

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

# publications[].label
Compressible boundary layers over wavy walls

# publications[].label
Laminar Flow Control Flight Experiment Design and Execution

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

# publications[].label
Design of an Infinite-Swept-Wing Glove for In-Flight Discrete-Roughness-Element Experiment

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

# publications[].label
A flight test technique for precise angle-of-attack measurements with application to laminar flow control flight research

# publications[].label
Experiments on the subharmonic route to turbulence in boundary layers.

# publications[].label
A Transonic Laminar-Flow Wing Glove Flight Experiment: Overview and Design Optimization

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

# publications[].label
Secondary instability of crossflow vortices

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

# publications[].label
Swept-Wing Boundary-Layer Transition and Turbulent Flow Physics from Multipoint Measurements

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

# publications[].label
Wavelength selection and growth of Goertler vortices

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

# publications[].label
FORCED AND UNFORCED SUBHARMONIC RESONANCE IN BOUNDARY-LAYER TRANSITION.

# publications[].label
Attachment-line heating in a compressible flow

# publications[].label
A Flight Test Technique for Precise Angle-of-Attack Measurements with Application to Laminar Flow Control Flight Research

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

# publications[].label
Boundary-layer receptivity of sound with roughness

# publications[].label
Design of a Swept-Wing Laminar Flow Control Flight Experiment for Transonic Aircraft

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

# publications[].label
Swept-wing laminar flow control studies using Cessna O-2A test aircraft

# publications[].label
Experiments in nonlinear saturation of stationary crossflow vortices in a swept-wing boundary layer

# publications[].label
Formation of three-dimensional structures on the transition to turbulence in boundary layers

# publications[].label
Boundary-layer receptivity of sound with roughness

# publications[].label
WAVELENGTH SELECTION AND TOTAL GROWTH OF GORTLER VORTICES.

# publications[].label
Roughness receptivity in swept-wing boundary layers - experiments

# publications[].label
Control of random disturbances in a boundary layer

# publications[].label
NONPARALLEL STABILITY OF BOUNDARY-LAYER FLOWS.

# publications[].label
High-bandwidth optical measurements of the second-mode instability in a Mach 6 Quiet Tunnel

# publications[].label
Interactive Computations and Experiments in Stability and Transition Research

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

# publications[].label
Computational Investigation of Step Excrescence Sensitivity in a Swept-Wing Boundary Layer

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

# publications[].label
Effects of suction on the Goertler instability of boundary layers

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

# publications[].label
Boundary-layer transition detection and structure identification through surface shear-stress measurements

# publications[].label
Leading-edge receptivity to sound - Experiments, DNS, theory

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

# publications[].label
Nonparallel stability of boundary-layer flows

# publications[].label
Stability of circular Couette flow of binary mixtures

# publications[].label
Nonlinear boundary layer receptivity with high-amplitude noise

# publications[].label
Robust, automated processing of IR thermography for quantitative boundary-layer transition measurements

# publications[].label
Spatiotemporal structure of a millimetric annular dielectric barrier discharge plasma actuator

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

# publications[].label
Computational Investigation of the Effects of Surface Imperfections and Excrescences on the Crossflow Instability

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

# publications[].label
An Analysis of Asymmetric Rolling Bodies with Nonlinear Aerodynamics

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

# publications[].label
NONPARALLEL STABILITY OF BOUNDARY LAYERS WITH PRESSURE GRADIENTS AND SUCTION.

# publications[].label
Roughness receptivity in swept-wing boundary layers  computations

# publications[].label
A multi-point correlation analysis of a crossflow-dominated boundary layer

# publications[].label
Computations for laminar flow control in swept-wing boundary layers

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

# publications[].label
Aircraft suitability model applied to a laminar flow control flight experiment

# publications[].label
Non-linear acoustic response of a spherical bubble

# publications[].label
Insight into swept wing boundary-layer transition and turbulent flow physics from multi-point measurements

# publications[].label
Nonlinear waves in a Kelvin-Helmholtz flow

# publications[].label
Effects of Step Excrescences on Swept-Wing Transition

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

# publications[].label
Linear Stability Theory Applied to Boundary Layers

# publications[].label
Laminar flow control flight experiment design and execution

# publications[].label
Nonlinear Stability and Transition in 3-D Boundary Layers

# publications[].label
Experimental study of crossflow instability on a mach 6 yawed cone

# publications[].label
Experiments on Discrete Roughness Element Technology for Swept-Wing Laminar Flow Control

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

# publications[].label
ORTHOGONAL COORDINATE GRID FOLLOWING THE THREE-DIMENSIONAL VISCOUS FLOW OVER A CONCAVE SURFACE.

# publications[].label
Flight Test Experiments on Discrete Roughness Element Technology for Laminar Flow Control

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

# publications[].label
Generation of crossflow vortices in a three-dimensional flat-plate flow.

# publications[].label
Role of Micron - Sized Roughness in Swept - Wing Transition

# publications[].label
Boundary-layer transition to turbulence: the last five years.

# publications[].label
Computational Investigation of Step Excrescence Sensitivity in a Swept-Wing Boundary Layer

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

# publications[].label
Leading-edge roughness as a transition control mechanism

# publications[].label
Computational Fluid Dynamics Validation Issues in Transition Modeling

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

# publications[].label
Experiments on leading-edge receptivity to sound

# publications[].label
Application of multi-point correlation techniques to aerodynamic flows

# publications[].label
EXPERIMENTS ON THE STABILITY OF CROSSFLOW VORTICES IN SWEPT-WING FLOWS.

# publications[].label
Effects of Step-Excrescence Location on Swept-Wing Transition

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

# publications[].label
Boundary-layer receptivity to freestream disturbances and its role in transition

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

# publications[].label
Laminar-Turbulent Transition on a Swept Wing

# publications[].label
Infrared thermography investigations in transitional supersonic boundary layers

# publications[].label
Laminar flow control flight tests for swept wings: Strategies for LFC

# 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

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

# etdChairOf[].label
Hedderman, Simon Peter (2013-01). Developments for a Swept Wing Airfoil to Study the Effects of Step and Gap Excrescences on Boundary Layer Transition. Master's Thesis.

# etdChairOf[].label
Carpenter, Andrew L. (2010-01). In-flight Receptivity Experiments on a 30-degree Swept-wing using Micron-sized Discrete Roughness Elements. Doctoral Dissertation.

# etdChairOf[].label
McKnight, Christopher William (2006-10). Design and safety analysis of an in-flight, test airfoil. Master's Thesis.

# etdChairOf[].label
Crawford, Brian Keith (2015-01). Laminar-Turbulent Transition Due to 2-D Excrescences at 1% Chord on a Swept Wing. Doctoral Dissertation.

# etdChairOf[].label
Hunt, Lauren Elizabeth (2012-02). Boundary-Layer Receptivity to Three-Dimensional Roughness Arrays on a Swept-Wing. Doctoral Dissertation.

# etdChairOf[].label
Schouten, Shane Michael (2008-10). Complete CFD analysis of a Velocity XL-5 RG with flight-test verification. Master's Thesis.

# etdChairOf[].label
Hofferth, Jerrod William (2013-05). Boundary-Layer Stability and Transition on a Flared Cone in a Mach 6 Quiet Wind Tunnel. Doctoral Dissertation.

# etdChairOf[].label
Craig, Stuart A (2015-04). Stability of High-Speed, Three-Dimensional Boundary Layers. Doctoral Dissertation.

# etdChairOf[].label
Duncan, Jr., Glen T. (2014-08). The Effects of Step Excrescences on Swept-Wing Boundary-Layer Transition. Doctoral Dissertation.

# etdChairOf[].label
West, David Edward (2014-12). Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements. Master's Thesis.

# etdChairOf[].label
Fanning, Joshua 1987- (2012-11). In-Flight Measurements of Freestream Atmospheric Turbulence Intensities. Master's Thesis.

# etdChairOf[].label
West, David Edward (2014-12). Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements. Master's Thesis.

# etdChairOf[].label
Woodruff, Matthew Jeffery (2012-07). Receptivity Studies on a Swept-Wing Model. Master's Thesis.

# etdChairOf[].label
Belisle, Michael Joseph (2013-11). Aerodynamic Design for Swept-wing Laminar Flow. Doctoral Dissertation.

# etdChairOf[].label
Williams, Thomas 1987- (2012-08). Design of an Instrumentation System for a Boundary Layer Transition Wing Glove Experiment. Master's Thesis.