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Christoph Hader
Assistant Professor, Aerospace-Mechanical Engineering | Member of the Graduate Faculty
Aerospace & Mechanical Engr
Map Page
Research Area
fluid dynamics,
aerodynamics,
boundary-layer transition,
numerical simulations,
hypersonic flow,
boundary layers,
numerical simulation,
nonlinear dynamics,
boundary layer,
hypersonic,
shock waves,
hypersonic aerodynamics,
heat transfer,
numerical methods,
mach 6,
aerospace engineering,
turbulence,
high-speed flow,
computational fluid dynamics,
wave propagation,
flow control,
random disturbances
Grants
(4)
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Publications
(59)
Recent
Direct Numerical Simulations of the Nonlinear Boundary Layer Transition Regime on a Blunt Swept Flat Plate at Mach 6
2023
boundary layers,
numerical simulations
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
Local Transition Model for Crossflow Instability in High-Speed Boundary-Layers
2023
boundary layers,
instability,
transition model,
crossflow,
high-speed
Data-Driven Mori-Zwanzig: Approaching a Reduced Order Model for Hypersonic Boundary Layer Transition
2023
data-driven modeling,
hypersonic aerodynamics,
reduced order model,
boundary-layer transition,
fluid dynamics
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
Numerical Investigations of Nonlinearly Generated Disturbance Waves in High-Speed Boundary Layers
2023
fluid dynamics,
turbulence,
wave dynamics,
boundary layers,
numerical simulations
Mori-Zwanzig Modal Decomposition
2023
mori-zwanzig,
data analysis,
fluid dynamics,
statistical mechanics
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
Collaborations
(4)
Jesse Little
Mutual work: 2 Proposals﹒2 Grants﹒1 Publication
Collaboration Details
Alex Craig
Mutual work: 1 Publication
Collaboration Details
Hermann Fasel
Mutual work: 4 Grants﹒6 Proposals﹒2 Techs
Collaboration Details
James Threadgill
Mutual work: 5 Proposals﹒3 Grants﹒1 Publication
Collaboration Details
Courses
(1)
Computer Programming in Aerospace and Mechanical Engineering
Techs/Patents
(2)
Flow Control Techniques For Delaying Or Accelerating Laminar-Turbulent Boundary-Layer Transition For High-Speed Flight Vehicles
2024
·
Patent
Control (Delay or Accelerate) Hypersonic Boundary-Layer Transition
2019
·
Technology
$62.6K / $2M Funding
50+ Publications
