关注
Robert Miller
Robert Miller
其他姓名Robert S. Miller, R. S. Miller
Professor of Engineering
在 uwa.edu 的电子邮件经过验证
标题
引用次数
引用次数
年份
OH* chemiluminescence imaging of the combustion products from a methane-fueled rotating detonation engine
J Tobias, D Depperschmidt, C Welch, R Miller, M Uddi, AK Agrawal, ...
Journal of Engineering for Gas Turbines and Power 141 (2), 021021, 2019
482019
Time-resolved PIV diagnostics to measure flow field exiting methane-fueled rotating detonation combustor
D Depperschmidt, R Miller, J Tobias, M Uddi, AK Agrawal, JB Stout
AIAA Scitech 2019 Forum, 1514, 2019
322019
Experimental analysis of wave propagation in a methane-fueled rotating detonation combustor
C Welch, D Depperschmidt, R Miller, J Tobias, M Uddi, AK Agrawal, ...
Turbo Expo: Power for Land, Sea, and Air 51067, V04BT04A065, 2018
322018
Rainbow schlieren imaging of density field in the exhaust flow of rotating detonation combustion
R Miller, J Tobias, D Depperschmidt, K Bell, D Langner, AK Agrawal
AIAA Propulsion and Energy 2019 Forum, 4380, 2019
162019
Design and Implementation of a Disk-Shaped Radial Rotating Detonation Engine with Integrated Aerospike
D Langner, A Gupta, R Miller, AK Agrawal
AIAA SciTech 2022 Forum, 0642, 2022
152022
Flow Measurements Inside a Rotating Detonation Combustor
J Tobias, R Miller, AK Agrawal
AIAA Propulsion and Energy 2020 Forum, 3869, 2020
132020
Uddi., M., Agrawal, AK, Stout, JB, Time-Resolved PIV Diagnostics to Measure Flow Field Exiting Methane-Fueled Rotating Detonation Combustor
D Depperschmidt, J Tobias, R Miller
AIAA-2019-1514, Presented at AIAA SciTech Forum 2019, San Diego, California, 2019
72019
Time-resolved PIV measurements of flow field at the exit of a diffuser mounted on a rotating detonation combustor
D Depperschmidt, J Tobias, R Miller, AK Agrawal
AIAA Propulsion and Energy 2019 Forum, 4379, 2019
62019
Imaging Exhaust Flow of Radial RDE using Rainbow Schlieren Deflectometry
A Gupta, D Langner, R Miller, S Sawaya, AK Agrawal
AIAA SCITECH 2023 Forum, 2391, 2023
52023
Effect of a Diffuser on Conditioning Flow Field Fluctuations at the Exit of a Rotating Detonation Combustor
J Tobias, D Depperschmidt, R Miller, M Uddi, AK Agrawal
Aerojet Rocketdyne, Sacramento, CA (United States), 2019
12019
Time-Resolved PIV Measurements of Flow Field at Diffuser Exit Downstream of a Rotating Detonation Combustor
DL Depperschmidt, JR Tobias, RS Miller, AK Agrawal
Aerojet Rocketdyne, Sacramento, CA (United States), 2019
2019
Flow Measurements of Methane-Fueled Rotating Detonation Combustion
D Depperschmidt, J Tobias, R Miller, M Uddi, A Agrawal, J Stout
Aerojet Rocketdyne, Sacramento, CA (United States), 2018
2018
Exit Flow Field of Methane-Fueld Rotating Detonation Engine Measured by Time Resolved Particle Image Velocimetry
D Depperschmidt, J Tobias, R Miller, M Uddi, A Agrawal
Aerojet Rocketdyne, Sacramento, CA (United States), 2018
2018
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