Phil Kreth
Phil Kreth
The University of Tennessee Space Institute (UTSI)
Verified email at - Homepage
Cited by
Cited by
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
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
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
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
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
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
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
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
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
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
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
Using high-frequency pulsed supersonic microjets to control resonant high-speed cavity flows
PA Kreth, FS Alvi
AIAA Journal 58 (8), 3378-3392, 2020
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
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
Velocity field measurements on high-frequency, supersonic microactuators
PA Kreth, MY Ali, EJ Fernandez, FS Alvi
Experiments in Fluids 57, 1-13, 2016
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
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
An Investigation of the Role of an Upstream Burst Diaphragm on Flow Quality within a Ludwieg tube using RANS
SA Lindörfer, P Anusonti-Inthra, CS Combs, PA Kreth, JD Schmisseur
46th AIAA Fluid Dynamics Conference, 3801, 2016
Shockwave/boundary-layer interaction studies performed in the NASA Langley 20-Inch Mach 6 Air Tunnel
BF Bathel, SB Jones, AN Watkins, S Berry, K Goodman, CS Combs, ...
AIAA Aviation 2019 Forum, 2904, 2019
Control of high frequency microactuators using active structures
PA Kreth, FS Alvi, BM Reese, WS Oates
Smart Materials and Structures 24 (2), 025030, 2015
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