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Phil Kreth
Phil Kreth
Associate Professor at the University of Tennessee
Verified email at utsi.edu - Homepage
Title
Cited by
Cited by
Year
Investigating unsteady dynamics of cylinder-induced shock-wave/transitional boundary-layer interactions
CS Combs, EL Lash, PA Kreth, JD Schmisseur
AIAA journal 56 (4), 1588-1599, 2018
532018
Image-based analysis of shock-wave/boundary-layer interaction unsteadiness
CS Combs, PA Kreth, JD Schmisseur, EL Lash
AIAA journal 56 (3), 1288-1293, 2018
362018
Design and initial characterization of the UTSI Mach 4 Ludwieg tube
PA Kreth, M Gragston, K Davenport, JD Schmisseur
AIAA Scitech 2021 Forum, 0384, 2021
322021
Developing an Image-Based Analysis of the Dynamics of Transitional Shock Wave-Boundary Layer Interactions
EL Lash, CS Combs, PA Kreth, EA Beckman, JD Schmisseur
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 4320, 2016
292016
Measurement of supersonic jet screech with focused laser differential interferometry
TJ Price, M Gragston, JD Schmisseur, PA Kreth
Applied Optics 59 (28), 8902-8908, 2020
272020
Study of the dynamics of transitional shock wave-boundary layer interactions using optical diagnostics
EL Lash, CS Combs, PA Kreth, JD Schmisseur
47th AIAA Fluid Dynamics Conference, 3123, 2017
272017
Experimental investigation of a cylinder-induced transitional shock wave-boundary layer interaction
EL Lash, CS Combs, PA Kreth, JD Schmisseur
55th AIAA Aerospace Sciences Meeting, 0760, 2017
252017
Modal analysis of cylinder-induced transitional shock-wave/boundary-layer interaction unsteadiness
ENA Hoffman, JM Rodriguez, SM Cottier, CS Combs, BF Bathel, ...
AIAA journal 60 (5), 2730-2748, 2022
232022
Laser differential interferometry and schlieren as an approach to characterizing freestream disturbance levels
AJ Harris, PA Kreth, CS Combs, JD Schmisseur
2018 AIAA Aerospace Sciences Meeting, 1100, 2018
222018
Characterization of Temperature Sensitive Paint for Application in Hypersonic Ludwieg Tubes at the University of Tennessee
C Smith, PA Kreth, JD Schmisseur, G Strickland
AIAA SCITECH 2022 Forum, 1660, 2022
192022
Numerical simulations of a cylinder-induced shock wave/boundary layer interaction
SA Lindörfer, CS Combs, PA Kreth, JD Schmisseur
55th AIAA Aerospace Sciences Meeting, 0534, 2017
192017
Using high-frequency pulsed supersonic microjets to control resonant high-speed cavity flows
PA Kreth, FS Alvi
AIAA Journal 58 (8), 3378-3392, 2020
172020
Microjet based active flow control on a fixed wing UAV
P Kreth, F Alvi, V Kumar, R Kumar
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2010
162010
Scaling of cylinder-generated shock-wave/turbulent boundary-layer interactions
SA Lindörfer, CS Combs, PA Kreth, RB Bond, JD Schmisseur
Shock Waves 30 (4), 395-407, 2020
152020
Characterizing the streamwise development of surface roughness effects on a supersonic boundary layer
BD Kocher, CS Combs, PA Kreth, JD Schmisseur
2018 Fluid Dynamics Conference, 4047, 2018
152018
Design and Initial Characterization of the UTSI Mach 7 Ludwieg Tube
M Gragston, K Davenport, F Siddiqui, N Webber, CD Smith, PA Kreth, ...
AIAA SCITECH 2023 Forum, 1457, 2023
132023
Velocity field measurements on high-frequency, supersonic microactuators
PA Kreth, MY Ali, EJ Fernandez, FS Alvi
Experiments in Fluids 57, 1-13, 2016
132016
Investigation of the effects of distributed surface roughness on supersonic flows
BD Kocher, CS Combs, PA Kreth, JD Schmisseur, SJ Peltier
47th AIAA Fluid Dynamics Conference, 4313, 2017
12*2017
Characterizing Streamwise Development of Surface Roughness Effects on a Supersonic Boundary Layer
BD Kocher, PA Kreth, JD Schmisseur, EJ LaLonde, CS Combs
AIAA Journal 60 (9), 5136-5149, 2022
102022
Simulations of Dynamic Shock Wave/Boundary Layer Interactions Using HPCMP CREATETM-AV Kestrel COFFE
NF Nutter, JW Cobourn, RB Bond, PA Kreth, JD Schmisseur, RS Glasby, ...
AIAA Scitech 2021 Forum, 0499, 2021
102021
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