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Christoph Hader
Assistant Professor, Aerospace-Mechanical Engineering | Member of the Graduate Faculty
Aerospace & Mechanical Engr
Map Page
Research Area
aerodynamics,
fluid dynamics,
boundary-layer transition,
numerical simulations,
hypersonic flow,
numerical simulation,
nonlinear dynamics,
boundary layer,
boundary layers,
mach 6,
shock waves,
hypersonic aerodynamics,
hypersonic,
aerospace engineering,
high-speed flow,
numerical methods,
heat transfer,
computational fluid dynamics,
wave propagation,
turbulence,
wing design,
flow control,
random disturbances
Grants
(4)
Optical Glass and Precise Mach Number Control for the Transonic Portion of the Arizona Polysonic Wind Tunnel
Active
·
2024
·
$62.6K / $189.7K
·
External
Co-Investigator (COI)
optical glass,
transonic,
wind tunnel,
mach number control,
precision machining
Separation Bubble Dynamics: A Comprehensive Investigation of Low- and High-Speed Flows using Experiments, Simulations, and Stability Theory
Active
·
2023
·
$0 / $798.2K
·
External
fluid dynamics,
computational fluid dynamics,
stability theory,
aerodynamics
Investigation of Transitional SBLI at Mach 5 using Controlled Forcing: Experiments, Simulations and Theory
Active
·
2023
·
$0 / $322.7K
·
External
Co-Investigator (COI)
transitional flow,
shock boundary layer interaction,
mach 5,
controlled forcing,
experiments
Numerical Investigations of the Nonlinear Transition Stages in Boundary Layers for High Mach Numbers
Active
·
2022
·
$0 / $550.9K
·
External
numerical simulations,
boundary layers,
nonlinear dynamics,
high mach numbers,
transition stages
Publications
(59)
Recent
Numerical Investigations of Nonlinearly Generated Disturbance Waves in High-Speed Boundary Layers
2023
fluid dynamics,
boundary layer,
nonlinear waves,
numerical simulation,
turbulence modeling
Schlieren Visualization of Controlled Disturbances in Mach 5 Flow Over a Hollow Cylinder Flare
2023
aerodynamics,
fluid dynamics,
schlieren imaging,
hypersonic flow,
flow control
Numerical Investigations of Hypersonic Boundary-Layer Stability for a Blunt Flat Delta Wing
2023
aerodynamics,
boundary-layer stability,
hypersonics,
numerical simulations,
wing design
Data-Driven Mori-Zwanzig: Reduced Order Modeling of Sparse Sensors Measurements for Boundary Layer Transition
2023
data-driven modeling,
reduced order modeling,
boundary-layer transition,
sparse sensors,
mori-zwanzig
Mori-Zwanzig Modal Decomposition
2023
modal decomposition,
mori-zwanzig,
fluid dynamics,
data analysis,
nonlinear dynamics
Direct Numerical Simulations of the Nonlinear Boundary Layer Transition Regime on a Blunt Swept Flat Plate at Mach 6
2023
boundary-layer transition,
numerical simulations,
fluid dynamics,
aerodynamics,
swept flat plate
Numerical investigation of the laminar-turbulent boundary-layer transition for a circular cone at Mach 5: wind tunnel and flight conditions
2023
aerodynamics,
boundary layers,
fluid dynamics,
aerospace engineering,
wind tunnel testing
Modal Analysis with Mori-Zwanzig Formalism: Application to Hypersonic Boundary Layer Flow
2023
modal analysis,
mori-zwanzig formalism,
hypersonic flow,
boundary layer,
application
Machine-Learning-Based Transition Prediction for Hypersonic Boundary Layers with Crossflow
2023
machine learning,
hypersonic,
boundary layers,
transition prediction,
crossflow
Experimental measurements and numerical investigations of boundary-layer instabilities on a Mach 5 hollow cylinder
2023
fluid dynamics,
boundary-layer instabilities,
high-speed flow,
aerodynamics,
thermal management
Collaborations
(4)
Jesse Little
Mutual work: 2 Grants﹒2 Proposals﹒1 Publication
Collaboration Details
Alex Craig
Mutual work: 1 Publication
Collaboration Details
Hermann Fasel
Mutual work: 4 Grants﹒2 Techs﹒6 Proposals
Collaboration Details
James Threadgill
Mutual work: 3 Grants﹒1 Publication﹒5 Proposals
Collaboration Details
Courses
(1)
Computer Programming in Aerospace and Mechanical Engineering
Techs/Patents
(2)
Control (Delay or Accelerate) Hypersonic Boundary-Layer Transition
2019
·
Technology
Flow Control Techniques For Delaying Or Accelerating Laminar-Turbulent Boundary-Layer Transition For High-Speed Flight Vehicles
1899
·
Patent
$62.6K / $1.9M Funding
50+ Publications
