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Hermann Fasel
Member of the Graduate Faculty | Professor, Aerospace-Mechanical Engineering
Aerospace & Mechanical Engr
Map Page
Research Area
aerodynamics,
fluid dynamics,
boundary layer,
numerical simulations,
turbulence,
numerical simulation,
boundary-layer transition,
boundary layers,
hypersonic flow,
computational fluid dynamics,
hypersonic,
aerospace engineering,
flow control,
laminar flow,
fluid mechanics,
wind tunnel testing,
renewable energy,
numerical methods,
shock waves,
laminar-turbulent transition,
hypersonic aerodynamics,
turbulence modeling,
hypersonics,
control systems,
transition,
wing design,
supersonic flow,
stability analysis,
structural dynamics,
thermal engineering
Grants
(51)
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
·
$399.1K / $798.2K
·
External
Co-Investigator (COI)
fluid dynamics,
computational fluid dynamics,
stability theory,
aerodynamics
Investigation of Transitional SBLI at Mach 5 using Controlled Forcing: Experiments, Simulations and Theory
Active
·
2023
·
$161.4K / $322.7K
·
External
Co-Investigator (COI)
transitional flow,
shock boundary layer interaction,
mach 5,
controlled forcing,
experiments
A Combined Approach for Investigating the Effects of Large Wing Sweep and Unsteady Wing Motion on Transition and Separation: Flight Experiments, Wind Tunnel Experiments and Simulations
Active
·
2023
·
$192K / $320K
·
External
Principal Investigator (PI)
aerodynamics,
flight testing,
wing motion,
wind tunnel testing,
fluid dynamics
Numerical Investigations of the Nonlinear Transition Stages in Boundary Layers for High Mach Numbers
Active
·
2022
·
$550.9K
·
External
Principal Investigator (PI)
numerical simulations,
boundary layers,
nonlinear dynamics,
high mach numbers,
transition stages
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Publications
(312)
Recent
Transition Model for Second Mode and Crossflow Instabilities in Hypersonic Flow
2024
hypersonic flow,
instabilities,
transition model,
second mode,
crossflow
Numerical investigations of laminar-turbulent transition for a hollow cylinder flare at Mach 5
2024
aerodynamics,
turbulence,
thermal effects,
material science,
fluid dynamics
Scaling and Transition Effects on Hollow-Cylinder/Flare SBLIs in Wind Tunnel Environments
2024
fluid dynamics,
wind tunnel testing,
transition effects,
shock boundary layer interactions,
aerodynamics
Numerical Investigation of Hypersonic Boundary-Layer Transition for an Ogive Geometry
2024
aerodynamics,
hypersonics,
boundary layer,
numerical modeling,
transition phenomena
Effects of Small Leading-Edge Bluntness on High-Speed Boundary-Layer Instabilities on Flat Plates
2024
aerodynamics,
boundary layers,
instabilities,
bluntness,
high-speed
Investigation of Cross-Flow in the Presence of a Laminar Separation Bubble
2024
fluid dynamics,
turbulence,
boundary layer,
aerodynamics,
separation phenomena
Schlieren Visualization of Controlled Disturbances in Mach 5 Flow Over a Hollow Cylinder Flare
2023
aerodynamics,
fluid dynamics,
schlieren imaging,
hypersonic flow,
flow control
Mori-Zwanzig Modal Decomposition
2023
modal decomposition,
mori-zwanzig,
fluid dynamics,
data analysis,
nonlinear dynamics
Numerical Investigations of Nonlinearly Generated Disturbance Waves in High-Speed Boundary Layers
2023
fluid dynamics,
boundary layer,
nonlinear waves,
numerical simulation,
turbulence modeling
Modal Analysis with Mori-Zwanzig Formalism: Application to Hypersonic Boundary Layer Flow
2023
modal analysis,
mori-zwanzig formalism,
hypersonic flow,
boundary layer,
application
Collaborations
(24)
Salim Hariri
Mutual work: 3 Proposals
Collaboration Details
Michael Chertkov
Mutual work: 1 Proposal
Collaboration Details
Roberto Furfaro
Mutual work: 1 Proposal
Collaboration Details
Jesse Little
Mutual work: 35 Proposals﹒2 Publications﹒16 Grants
Collaboration Details
Krishna Muralidharan
Mutual work: 1 Proposal
Collaboration Details
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News
(10)
Investigating Boundary Layers in Hypersonic Flight
2021
$1.5M Advances Hypersonics Research and Technology
2021
Modifications Elevate Wind Tunnel Capacity – From Subsonic to Hypersonic
2020
UA Engineers Tackle Hypersonic Flight
2017
UA Engineering Professor Wins Air Force Grant
2015
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Courses
(4)
Numerical Methods in Fluid Mechanics and Heat Transfer
Hydrodynamic Stability
Advanced Computational Aerodynamics
Aircraft Performance
Techs/Patents
(4)
Control of Hypersonic Boundary Layer Transition
2021
·
Patent
Control (Delay or Accelerate) Hypersonic Boundary-Layer Transition
2019
·
Technology
Control of Boundary-Layer Transition for Hypersonic Flight
2015
·
Technology
Flow Control Techniques For Delaying Or Accelerating Laminar-Turbulent Boundary-Layer Transition For High-Speed Flight Vehicles
1899
·
Patent
20+ Collaborators
$15.5M / $23M Funding
50+ Grants
310+ Publications
9+ News
