Institutional Knowledge Map (KMap)
Map
Services
How To Use
About
Toggle theme
Loading...
Menu
Jesse Little
Adjunct Research Professor, Aerospace-Mechanical Engineering
Aerospace & Mechanical Engr
Map Page
Research Area
aerodynamics,
fluid dynamics,
boundary layer,
flow control,
shock waves,
turbulence,
aircraft design,
control systems,
aerospace engineering,
plasma actuators,
aerospace,
plasma physics,
wing design,
airfoil,
dielectric barrier discharge,
mechanical engineering,
separation control,
wind tunnel,
wind tunnel testing,
oblique shock,
turbulent flows,
structural dynamics,
turbulent mixing,
shock wave,
aeronautics,
numerical simulations,
testing
Grants
(46)
Sign in to view all grants
Page 1 of 10
Previous page
Next page
Publications
(68)
Recent
Fin-induced Shock Boundary Layer Interactions on a Flat Plate and Hollow Cylinder at Mach 5
2022
shock boundary layer,
aerodynamics,
boundary layer interaction,
aerospace engineering,
fluid dynamics
Flow Similarity in Swept Shock/Boundary Layer Interactions
2022
flow similarity,
shock waves,
boundary layer,
swept interactions,
fluid dynamics
An inviscid analysis of swept oblique shock reflections
2020
shock reflections,
inviscid analysis,
swept,
oblique shock,
aerodynamics
Experimental Study of Swept Impinging Oblique Shock/Boundary-Layer Interactions
2020
fluid dynamics,
aerodynamics,
boundary-layer interactions,
shock waves
A comparative study of Ac-dielectric barrier discharge versus Ns-dielectric barrier discharge plasma actuators in an incompressible turbulent mixing layer
2020
plasma actuators,
turbulent mixing,
dielectric barrier discharge,
incompressible flow
Parametric study of Ns-DBD plasma actuators in a turbulent mixing layer
2020
plasma actuator,
turbulent mixing,
aerodynamics,
fluid mechanics
Post-stall flow control using nanosecond pulse driven dielectric barrier discharge plasma actuators
2019
fluid dynamics,
plasma physics,
aeronautics,
nanotechnology,
control engineering
Comparison Between Fluidic Oscillators and Steady Jets for Separation Control
2019
fluidic oscillators,
steady jets,
separation control,
comparison,
fluid dynamics
Comparison of Various Fluidic Oscillators for Separation Control on a Wall-Mounted Hump
2019
fluid dynamics,
separation control,
wall-mounted,
fluidic oscillators,
comparison
Transitional Shock Wave Boundary Layer Interactions on a Compression Ramat Mach 4
2019
aerodynamics,
boundary layer,
shock waves,
compression ramp,
transitional flow
Collaborations
(33)
Michael Chertkov
Mutual work: 1 Proposal
Collaboration Details
Roberto Furfaro
Mutual work: 4 Proposals
Collaboration Details
Regina Deil-Amen
Mutual work: 1 Proposal
Collaboration Details
Krishna Muralidharan
Mutual work: 2 Proposals
Collaboration Details
Alex Craig
Mutual work: 7 Grants﹒4 Publications﹒23 Proposals
Collaboration Details
Page 1 of 7
Previous page
Next page
News
(7)
$10M elevates UArizona hypersonics facilities to national prominence
2022
Investigating Boundary Layers in Hypersonic Flight
2021
$1.5M Advances Hypersonics Research and Technology
2021
Gov. Ducey Says Investment in Hypersonic Flight is Ticket to the Future
2021
Modifications Elevate Wind Tunnel Capacity – From Subsonic to Hypersonic
2020
Page 1 of 2
Previous page
Next page
Courses
(5)
Introduction to Aerospace Engineering
Senior Aerospace Laboratory
Aerodynamics
Nature of Turbulent Shear Flow
Introduction to Fluid Mechanics
30+ Collaborators
$8.7M / $13.5M Funding
40+ Grants
60+ Publications
4+ Courses
6+ News