# 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[]
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

# 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[]
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[]
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[]
Networking And Information Technology R&d (nitrd)

# keywords[]
Networking And Information Technology R&d

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4007 Control Engineering, Mechatronics And Robotics

# keywords[]
4007 Control Engineering, Mechatronics And Robotics

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
5102 Atomic, Molecular And Optical Physics

# keywords[]
4009 Electronics, Sensors And Digital Hardware

# 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

# 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
Goucher College - (Towson, Maryland, United States)

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

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

# awardsAndHonors[].label
William O. and Montine P. Head Faculty Fellow

# awardsAndHonors[].label
Association of Former Students University-Level Distinguished Achievement Award, The

# awardsAndHonors[].label
Association of Former Students University-Level Distinguished Achievement Award, The

# awardsAndHonors[].label
Thomas U. McElmurry Teaching Excellence Award

# awardsAndHonors[].label
Presidential Professor for Teaching Excellence Award

# awardsAndHonors[].label
Association of Former Students College-Level Teaching Distinguished Achievement Award, The

# awardsAndHonors[].label
Edward 'Pete' Aldridge '60 Professorship

# 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 flight tests for swept wings: Strategies for LFC

# publications[].label
PSE and Spatial Biglobal Instability Analysis of HIFiRE-5 Geometry

# 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
Microsatellite and formation flying technologies on university nanosatellites

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

# publications[].label
Drag prediction and transition in hypersonic flow

# 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
ASUSat3 (Digital Microfluidics Device and Micropropulsion Demonstrator)

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

# publications[].label
Parametric Boundary-Layer Stability Analysis on a Hypersonic Finned Circular Cone

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

# publications[].label
Spatial BiGlobal Stability Analysis of Spanwise Vortex Rollup on a Hypersonic Finned Cone

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

# publications[].label
Effect of suction and blowing on boundary-layer transition

# 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
Computations for laminar flow control in swept-wing boundary layers

# publications[].label
Boundary layer receptivity to free-stream vorticity

# publications[].label
Nonlinear Boundary-Layer Stability Analysis of BOLT and HIFiRE-5

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

# publications[].label
Stability of High-Speed Chemically Reacting and Three-Dimensional Boundary Layers

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

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

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

# publications[].label
FLOW OVER PLATES WITH SUCTION THROUGH POROUS STRIPS.

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

# publications[].label
Linear Stability of a Boundary-Layer Vortex on a Hypersonic Finned Cone

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

# publications[].label
Stability of three-dimensional supersonic boundary layers

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

# publications[].label
Hypersonic Stability and Transition Prediction

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

# publications[].label
Simulation of swept-wing vortices using nonlinear parabolized stability equations

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

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

# publications[].label
Cross-Flow Instability Experiments on a Swept Fin-Cone with Variable Nose Bluntness in Mach 6 Flow

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

# publications[].label
A Method to Determine the Performance of Low-Reynolds-Number Airfoils under Off-Design Unsteady Freestream Conditions

# 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
Disturbance-wave interactions in flows with crossflow

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

# publications[].label
Local intermodal energy transfer of the secondary instability in a plane channel

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

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

# publications[].label
Numerical-Experimental Comparisons of Second-Mode Behavior for Blunted Cones

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

# publications[].label
Verification and Validation Issues in Hypersonic Stability and Transition Prediction

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

# publications[].label
Grtler Instability on a Variably Swept, Slotted, Natural-Laminar-Flow Airfoil

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

# publications[].label
Pre-Flight Boundary-Layer Stability Analysis of BOLT Geometry

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

# publications[].label
JoKHeR: NPSE Simulations of Hypersonic Crossflow Instability

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

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

# publications[].label
Numerical simulations of transition in oscillatory plane channel flow

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

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

# publications[].label
Correction: DEKAF: spectral multi-regime basic-state solver for boundary layer stability

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

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

# publications[].label
A university microsatellite as a mems-based propulsion testbed

# publications[].label
Leading-Edge Receptivity to a Vortical Freestream Disturbance: A Numerical Analysis

# publications[].label
Secondary instability analysis of crossflow on a hypersonic yawed straight circular cone

# publications[].label
Leading-edge receptivity to oblique acoustic waves

# publications[].label
Progress in Stability and Transition Research

# publications[].label
Streamline - Curvature Effect in Three - Dimensional Boundary Layers

# 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
Development of the BOLT II Roughness Experiment for Flight

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

# 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
Observations in Using Linear Stability Theory for 3-D Supersonic Boundary Layers

# publications[].label
Boundary-Layer Stability Analysis on a Parametric Hypersonic Finned Circular Cone

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

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

# publications[].label
DISTURBANCE-WAVE INTERACTIONS IN FLOWS WITH CROSSFLOW.

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

# publications[].label
Direct numerical simulation of leading-edge receptivity to sound

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

# publications[].label
Flow over bodies with suction through porous strips

# publications[].label
Simulation of Laminar-Turbulent Transition in the Vicinity of a Wall.

# publications[].label
DNS of leading-edge receptivity to sound

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

# publications[].label
Linear disturbances in hypersonic, chemically reacting shock layers

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

# publications[].label
Analysis of the BOLT II - Holden Mission Flight and Wind Tunnel Geometries

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

# publications[].label
DEKAF: spectral multi-regime basic-state solver for boundary layer stability

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

# publications[].label
Numerical-Experimental Comparisons of Second-Mode Behavior for Blunted Cones

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

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

# publications[].label
The analysis of unsteady, three-dimensional flow separation

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

# publications[].label
Boundary-Layer Stability of a Natural-Laminar-Flow Airfoil

# 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
Dynamics and control of nanosatellite ASUSat1

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

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

# publications[].label
Asusat 1: An example of low-cost nanosatellite development

# 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
Boundary-Layer Instability on a Highly Swept Fin on a Hypersonic Cone

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

# publications[].label
Boundary-Layer Stability of a Natural-Laminar-Flow Airfoil at Flight Conditions

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

# publications[].label
Flow over Plates with Suction through Porous Strips

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

# publications[].label
Numerical model for circulation-control flows

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

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

# publications[].label
Preparing Effectively For Abet Accreditation: What Does It All Mean?

# publications[].publisher
American Society for Engineering Education

# publications[].label
Transition correlations in three-dimensional boundary layers

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

# publications[].label
Instability Analysis and Turbulent Transition Control of a Hypersonic Boundary Layer Developed Over a Swept Fin Cone Geometry in Mach 6 Flow

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

# publications[].label
FLOW OVER PLATES WITH SUCTION THROUGH POROUS STRIPS.

# publications[].label
Advances Laminar Flow Control on a Swept Wings - Useful crossflow Vortices and Suction

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

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

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

# publications[].label
Panel Session ET-03 - Space technology research in academia

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

# 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
Computational fluid dynamics validation issues in transition modeling

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

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

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

# publications[].label
The Ionospheric Plasma Research Experiment - ASUSat 1 and advanced spacecraft technology applications

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

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

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

# publications[].label
Computational Stability Analysis of a Variably Swept, Slotted Natural-Laminar-Flow Airfoil

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

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

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

# publications[].label
Effect of curvature on stationary crossflow instability of a three-dimensional boundary layer

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

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

# publications[].label
MarsCAT: Mars Array of ionospheric Research Satellites using the CubeSat Ambipolar Thruster

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

# publications[].label
Numerical Simulation of Transition in a Decelerating Boundary Layer

# publications[].label
Boundary-Layer Stability Analysis of HIFiRE-5b Flight Geometry

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

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

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

# publications[].label
Heat Transfer and Boundary-Layer Stability Analysis of Subscale BOLT and the Fin Cone

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

# publications[].label
Sensitivity of Second-Mode Linear Stability to Constitutive Models within Hypersonic Flow

# 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 (AIAA)

# publications[].label
Linear stability of supersonic cone boundary layers

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

# publications[].label
Nonlinear Boundary-Layer Stability Analysis of a Swept, Natural-Laminar-Flow Airfoil

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

# publications[].label
Linear Parabolized Stability Analysis of the BOLT Flight Geometry at Off-Nominal Conditions

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

# publications[].label
Assessment of the Amplification Factor Transport Transition Model for High-Mach Number Flows

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

# publications[].label
Investigation of the effects of initial disturbances on plane channel transition

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

# publications[].label
Ionization and dissociation effects on boundary-layer stability

# publications[].label
Stability, Transition, and Control of Three-Dimensional Boundary Layers on Swept Wings

# 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
Analysis of the BOLT Flight Geometry At Off-Nominal Conditions

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

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

# 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
Mechanisms for Control of Boundary-Layer Turbulence Across the Speed Regimes

# publications[].label
Stability of hypersonic chemically reacting viscous flows

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

# 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
Direct Numerical Simulation of Distributed Roughness on a Swept Wing Leading Edge

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

# publications[].label
Numerical-perturbation technique for stability of flat-plate boundary layers with suction

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

# publications[].label
Boundary Layer Stability Analysis of HIFiRE-5b Flight Geometry

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

# publications[].label
Boundary-Layer Stability of a Slotted, Natural-Laminar-Flow Airfoil at Flight Conditions

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

# publications[].label
Diffusion and chemical non-equilibrium effects on hypersonic boundary-layer stability

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

# publications[].label
Computational Optimization of a Natural Laminar Flow Experimental Wing Glove

# 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
Design of an Infinite Swept Wing Glove for an In-Flight DRE Experiment

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

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

# publications[].label
PSE and Spatial Biglobal Instability Analysis of Reduced Scale and Flight HIFiRE-5 Geometry

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

# publications[].label
Transition Mechanisms for Transport Aircraft

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

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

# publications[].label
The Langmuir Probe and Waves (LPW) Instrument for MAVEN

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

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

# publications[].label
Stability of flow over axisymmetric bodies with porous suction strips

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

# 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
Energy-Budget Analysis of the Crossflow Instability on a Hypersonic Yawed Cone

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

# publications[].label
Abet Accreditation: Best Practices For Assessment

# publications[].publisher
American Society for Engineering Education

# publications[].label
Arizona State University Satellite 1 (ASUSat1): Low-Cost, Student-Designed Nanosatellite

# 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
Effect of streamwise vortices on transition in plane-channel flow

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

# publications[].label
Accurate and Efficient Modeling of Boundary-Layer Instabilities

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

# publications[].label
Stability of Hypersonic Compression Cones

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

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

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

# publications[].label
Active Control of Unsteady Gasdynamics for Shock Compression and Turbulence Generation

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

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

# publications[].label
The effects of streamwise vortices on transition in the plane channel

# publications[].label
Use of transition correlations for three-dimensional boundary layers within hypersonic flows

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

# publications[].label
Integrated Theoretical, Computational, and Experimental Studies for Transition Estimation and Control

# 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
Laminar Flow Control on a Swept Wing with Distributed Roughness

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

# publications[].label
Comparative Studies on the Hypersonic Finned Cone

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

# publications[].label
Trimetric Imaging of the Martian Ionosphere Using a CubeSat Constellation

# 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
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
Numerical investigation of receptivity to freestream vorticity

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

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

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

# publications[].label
Use of transition correlations for three-dimensional boundary layers within hypersonic, viscous flows

# publications[].label
Application of a solution-adaptive method to fluid flow: Line and arclength approach

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

# 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
Numerical simulations of transition in oscillatory plane channel flow

# publications[].label
Direct Numerical Simulation of Leading-Edge Receptivity to Sound

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

# publications[].label
Flow over bodies with suction through porous strips

# publications[].label
Preflight Boundary-Layer Stability Analysis of BOLT Geometry

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

# publications[].label
UNSTEADY SEPARATION AT LOW REYNOLDS NUMBERS.

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

# publications[].label
Introduction: 13th Annual Gallery of Fluid Motion (Irvine, California, USA, 1995)

# 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
Stability limits for three-dimensional supersonic 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
Stability and control of high-speed 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
Computational modeling and stability analysis of BOLT hypersonic geometry including off-nominal conditions

# publications[].label
A university microsatellite as a MEMS-based propulsion testbed

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

# publications[].label
Bandwidth Effects on Mack-Mode Instability

# 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
Three-dimensional Stability of Boundary Layers

# publications[].label
Using the cubeSat Ambipolar Thruster to create a Mars Array of research satellites: MarsCAT

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

# 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
Correction: Interactive Computations and Experiments in Stability and Transition Research

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

# 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
CFD Validation Issues for Boundary-Layer Stability and Transition

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

# publications[].label
Numerical Modeling of the Free-Molecular Micro-Resistojet Prototype and Next Generation Designs Evaluation (Invited)

# 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
Stability of Three-Dimensional Boundary Layers

# publications[].label
ANALYSIS OF WAVE INTERACTIONS IN SWEPT-WING FLOWS.

# publications[].label
Stability of three-dimensional supersonic boundary layers

# publications[].label
EPIC: NPSE Analysis of Hypersonic Crossflow Instability on Yawed Straight Circular Cone

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

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

# publications[].label
AggieSat Laboratory SmallSat Controls Testbed

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

# publications[].label
Effect of Leading-Edge Geometry on Boundary-Layer Receptivity to Freestream Sound

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

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

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

# publications[].label
Relation of glaze ice formations on swept wings to crossflow instability

# publications[].label
Secondary Instability Analysis of Crossflow on a Hypersonic Yawed Straight Circular Cone

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

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

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

# publications[].label
Hypersonic Stability Analysis of a Flared Cone

# 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
Toward Practical Laminar Flow Control - Remaining Challenges

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

# publications[].label
ASUSat lab - Student projects in aerospace

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

# publications[].label
High-frequency instabilities along the windward face of a hypersonic yawed circular cone

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

# publications[].label
Correction: Pre-Flight Boundary-Layer Stability Analysis of BOLT Geometry

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

# publications[].label
Computational Aspects of Nonparallel Effects in Boundary-Layer Receptivity

# publications[].label
ASUSat1: the development of a low-cost satellite

# publications[].publisher
SPIE, the international society for optics and photonics

# publications[].label
Effects of Initial Disturbance Amplitude on Hypersonic Crossflow Instability

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

# publications[].label
High-enthalpy models for boundary-layer stability and transition

# publications[].label
Correction: Parametric Boundary-Layer Stability Analysis on a Hypersonic Finned Circular Cone

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

# publications[].label
Introduction: 12th Annual Gallery of Fluid Motion (Atlanta, Georgia, USA, 1994)

# publications[].label
Heat Flux on a Hypersonic Cone with a Highly Swept Fin

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

# publications[].label
INITIAL AND FEEDBACK SOLUTIONS FOR ORBITAL PURSUIT EVASION USING A HOMOTOPY METHOD

# publications[].label
2-D numerical model for predicting the aerodynamic performance of the NOTARTM system tailboom

# publications[].label
Introduction: 15th Annual Gallery of Fluid Motion (San Francisco, California, USA, 1997)

# publications[].label
Instabilities on a Hypersonic Yawed Straight Cone

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

# publications[].label
Sensitivity Methods Applied to Orbital Pursuit Evasion

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

# publications[].label
Numerical Simulation of Swept-Wing Vortices Using Nonlinear Parabolized Stability Equations

# 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
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[].awardedBy.label
United States Department of the Navy - (Arlington, Virginia, 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[].awardedBy.label
National Aeronautics and Space Administration - (Washington D.C., District of Columbia, United States)

# researcherOn[].label
AggieSat2: Autonomous Rendezvous and Docking

# researcherOn[].awardedBy.label
Johnson Space Center - (Houston, Texas, United States)

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

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

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

# inTheNews[].label
Texas A&M Announces 2020 Distinguished Achievement Award Recipients

# inTheNews[].label
Seven Texas A&M Faculty Members Awarded With University Distinguished Professorships

# etdChairOf[].label
Moyes, Alexander Jon (2019-08). Computational Laminar-to-Turbulent Transition Physics of Complex Three-Dimensional Hypersonic Flow Fields. Doctoral Dissertation.

# etdChairOf[].label
Kocian, Travis Scott (2018-05). Computational Hypersonic Boundary-Layer Stability and the Validation and Verification of EPIC. Doctoral Dissertation.

# etdChairOf[].label
Hafer, William Thomas (2014-08). Sensitivity Methods Applied to Orbital Pursuit-Evasion. Doctoral Dissertation.

# etdChairOf[].label
Stancliffe, Devin Aldin (2010-08). Analysis and Design of a Test Apparatus for Resolving Near-Field Effects Associated With Using a Coarse Sun Sensor as Part of a 6-DOF Solution. Master's Thesis.

# etdChairOf[].label
Roberts, Matthew William (2012-05). Computational Evaluation of a Transonic Laminar-Flow Wing Glove Design. Master's Thesis.

# etdChairOf[].label
Tucker, Aaron 1975- (2012-12). Laminar Flow Control Flight Experiment Design. Doctoral Dissertation.

# etdChairOf[].label
McLelland, Angela N (2013-12). Simulation and Experimental Predictionss for the Structural Response of Satellites. Master's Thesis.

# etdChairOf[].label
Neale, Tyler P. (2010-05). CFD Investigations of a Transonic Swept-Wing Laminar Flow Control Flight Experiment. Master's Thesis.

# etdChairOf[].label
Oliviero, Nick B (2015-05). EPIC: A New and Advanced Nonlinear Parabolized Stability Equation Solver. Master's Thesis.

# etdChairOf[].label
Rhodes, Richard G. (2008-12). Computations of Laminar Flow Control on Swept Wings as a Companion to Flight Test Research. Master's Thesis.

# etdChairOf[].label
Tufts, Matthew W (2015-12). Computational Investigation of Sensitivity of the Crossflow Instability to Two-Dimensional Surface Imperfections. Doctoral Dissertation.

# etdChairOf[].label
Goodnight, Ryan David (2009-08). An Innovative Approach for Data Collection and Handling to Enable Advancements in Micro Air Vehicle Persistent Surveillance. Master's Thesis.

# etdChairOf[].label
Graves, John (2011-12). Small Satellite Applications of Commercial off the Shelf Radio Frequency Integrated Circuits. Master's Thesis.

# etdChairOf[].label
Moyes, Alexander Jon (2019-06). Computational Laminar-to-Turbulent Transition Physics of Complex Three-Dimensional Hypersonic Flow Fields. Doctoral Dissertation.