Zobrazeno 1 - 7
of 7
pro vyhledávání: '"John M. Quinlan"'
Publikováno v:
AIAA SCITECH 2022 Forum.
Publikováno v:
AIAA Propulsion and Energy 2021 Forum.
Autor:
Ben T. Zinn, John M. Quinlan
Publikováno v:
AIAA Journal. 55:4314-4329
This paper describes a new approach that uses a small-scale rig, high-speed optical diagnostics, and the Krylov-based dynamic mode decomposition data analysis technique to elucidate the mechanisms ...
Publikováno v:
Journal of Propulsion and Power. 28:122-131
A predictive model for assessing the stabilization impact of radial blades, hub blade, and acoustic cavities in liquid propellant rocket engin es was developed, including nozzle, mean flow, and distributed combustion effects. A full t hree dimensiona
Autor:
Ben T. Zinn, John M. Quinlan
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
In this work we propose a new approach to elucidate specific combustion instability driving mechanisms and demonstrate application of the developed method to data collected using modern diagnostics. A laboratory-scale, optically accessible combustor
Autor:
Ben T. Zinn, John M. Quinlan
Publikováno v:
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
This paper discusses two new approaches for studying transverse acoustically coupled combustion instabilities in a laboratory environment. The mechanisms that drive combustion instabilities are frequency dependent, thus ideally would be studied in fu
Autor:
Timothy D. Hinerman, John M. Quinlan, Charles E. Mitchell, Whitney Rocketdyne, Allan Kirkpatrick, Dan Milano
Publikováno v:
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
High-frequency combustion instability in liquid propellant rocket engines, a coupling between the acoustics of the combustion chamber and the combustion process, remains a problem of significant interest. In this paper we analyze the combustion stabi