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Eugene Hoffman
Eugene Hoffman
Southwest Research Institute, University of Texas at San Antonio
在 swri.org 的电子邮件经过验证
标题
引用次数
引用次数
年份
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
162022
Design and Preliminary Calibration of the UTSA Mach 7 Hypersonic Ludwieg Tube
I Bashor, E Hoffman, G Gonzalez, CS Combs
AIAA Aviation 2019 Forum, 2859, 2019
162019
Characterization of the UTSA Mach 7 Ludwieg Tube
EN Hoffman, EJ LaLonde, M Garcia, V Delgado Elizondo, I Chen, H Bilbo, ...
AIAA SciTech 2022 Forum, 1600, 2022
152022
Velocity measurements in a hypersonic flow using acetone molecular tagging velocimetry
A Andrade, ENA Hoffman, EJ LaLonde, CS Combs
Optics Express 30 (23), 42199-42213, 2022
142022
Modal analysis of a sweeping jet emitted by a fluidic oscillator
DJ Portillo, EN Hoffman, M Garcia, E LaLonde, E Hernandez, CS Combs, ...
AIAA AVIATION 2021 FORUM, 2835, 2021
122021
Preliminary testing of the UTSA Mach 7 ludwieg tube
EN Hoffman, JM Rodriguez, M Garcia, V Delgado Elizondo, E LaLonde, ...
AIAA Aviation 2021 Forum, 2979, 2021
112021
Construction of a mach 7 ludwieg tube at UTSA
EN Hoffman, I Bashor, CS Combs
AIAA Aviation 2020 Forum, 2998, 2020
112020
Flow characterization of the UTSA hypersonic Ludwieg tube
ENA Hoffman, EJ LaLonde, A Andrade, I Chen, HA Bilbo, CS Combs
Aerospace 10 (5), 463, 2023
82023
Effects of surface roughness on shock-wave/turbulent boundary-layer interaction at Mach 4 over a hollow cylinder flare model
M Garcia, ENA Hoffman, EJ LaLonde, CS Combs, M Pohlman, C Smith, ...
Fluids 7 (9), 286, 2022
82022
Design considerations and analysis of the utsa hypersonic ludwieg tube facility
N Hoffman, CS Combs
AIAA Region IV Student Conference, 2019
72019
Effects of distributed roughness on shock-wave/boundary-layer interactions at Mach 7.2
EN Hoffman, DM Kendhammer, EJ LaLonde, A Andrade, CS Combs
AIAA SCITECH 2023 Forum, 0268, 2023
52023
Application of Pressure-Sensitive Paint to Investigate Hypersonic Shock-Wave/Boundary-Layer Interactions
A Andrade, EJ LaLonde, EN Hoffman, S Gutierrez, CS Combs
AIAA SCITECH 2023 Forum, 1178, 2023
52023
The Effects of Compressibility on the Performance and Modal Structures of a Sweeping Jet Emitted from Various Scales of a Fluidic Oscillator
DJ Portillo, E Hoffman, M Garcia, E LaLonde, C Combs, RL Hood
Fluids 7 (7), 251, 2022
32022
Global Surface Temperature Distribution on the Initial Concept 3. X Vehicle at Mach 7
A Dhanagopal, N Strasser, A Andrade, EN Hoffman, CS Combs
AIAA SCITECH 2024 Forum, 0668, 2024
22024
Validating Drag and Heating Coefficients for Hollow Reentry Objects in Continuum Flow Using a Mach 7 Ludwieg Tube
C Ostrom, J Marichalar, B Greene, A Andrade, ENA Hoffman, EJ LaLonde, ...
2nd International Orbital Debris Conference (IOD II), 2023
12023
Effects of Surface Roughness on Shock-Wave/Boundary-Layer Interactions at Mach 7.2
ENA Hoffman
The University of Texas at San Antonio, 2023
12023
Detonation cell size estimation via chemiluminescence imaging in an optically accessible linear detonation tube
BM Ng, ENA Hoffman, DI Pineda, CS Combs
Experiments in Fluids 65 (7), 108, 2024
2024
Thermal Evaluation of the Initial Concept 3. X Vehicle at Mach 7
A Dhanagopal, NS Strasser, A Andrade, KR Posladek, ENA Hoffman, ...
Energies 17 (12), 2916, 2024
2024
Flow Control of Hypersonic Shock-Wave/Boundary-Layer Interactions Using Phononic Metamaterials
JD Navarro, JCC Velasquez, EJ LaLonde, EN Hoffman, CS Combs, ...
AIAA SCITECH 2024 Forum, 0031, 2024
2024
Current Research in Experimental Aerodynamics at the UTSA Hypersonics Laboratory
JM Rodriguez, E Hoffman
NASA MIRO Peer Review Meeting, 2020
2020
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