Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Sarah Isert"'
Publikováno v:
Combustion and Flame. 183:322-329
Catalysts are often added to solid propellant formulations to tailor burning rates. Nanocatalysts can increase propellant burning rates over standard catalyst sizes due to the increase in surface area per unit weight. However, the increased surface a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cc011ba8ef0e7a0ee34e3032f9efa1a7
https://doi.org/10.1016/j.combustflame.2017.05.024
https://doi.org/10.1016/j.combustflame.2017.05.024
Publikováno v:
Proceedings of the Combustion Institute. 36:2283-2290
Tailoring solid propellant burning rates is a perpetual goal of solid propellant designers. Many methods have been used to alter the burning rate including changing the propellant formulation, adding burning rate modifiers, and changing the propellan
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::67a23f49ee2eed3baeb35dd3e92ada20
https://doi.org/10.1016/j.proci.2016.06.141
https://doi.org/10.1016/j.proci.2016.06.141
Autor:
Robert P. Lucht, Steven F. Son, Grant A. Risha, Trevor D. Hedman, Richard A. Yetter, Sarah Isert, Terry L. Connell
Publikováno v:
Combustion and Flame. 164:201-211
Simplified model propellant configurations, such as monomodal propellants, can be valuable in the development and validation of predictive numerical tools. These idealized experiments also yield insight into the effect of diffusion length scales on c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::78a3d554e1162c67aea8271a4e990ca6
https://doi.org/10.1016/j.combustflame.2015.11.017
https://doi.org/10.1016/j.combustflame.2015.11.017
Oxidizer coarse-to-fine ratio effect on microscale flame structure in a bimodal composite propellant
Publikováno v:
Combustion and Flame. 163:406-413
The microscopic flame structure of a composite propellant is expected to change significantly as the particle size distribution is varied. In this paper we report observations of the diffusion flame structures in burning ammonium perchlorate (AP) com
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e72c9c23de6f743f0c8fc51f85fa0536
https://doi.org/10.1016/j.combustflame.2015.10.015
https://doi.org/10.1016/j.combustflame.2015.10.015
Publikováno v:
Combustion and Flame. 162:1821-1828
In solid rocket propellants, nano-sized catalysts are expected to be more effective than their micron-sized counterparts due to their higher surface area and increased contact with the oxidizer. However, propellant processing becomes more difficult a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8b3a580b77841a2ead294057256dc252
https://doi.org/10.1016/j.combustflame.2014.11.040
https://doi.org/10.1016/j.combustflame.2014.11.040
Autor:
Sarah Isert, Steven F. Son
Publikováno v:
Challenges and Advances in Computational Chemistry and Physics ISBN: 9783319592060
The burning rate of a propellant is one of the most desired pieces of information for rocket motor design. Propellant burning rate is known to be linked to the microscale flame structures located just above the propellant surface. Flame structure and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b34376718e4423b2f812d3ab9c578cd1
https://doi.org/10.1007/978-3-319-59208-4_6
https://doi.org/10.1007/978-3-319-59208-4_6
Autor:
Ibrahim E. Gunduz, Travis R. Sippel, Sarah Isert, Brandon C. Terry, Steven F. Son, Lori J. Groven
Nanoscale metal fuels (e.g., aluminum) and ultra-high surface area catalysts promise improved performance over conventional ingredients in composite solid propellants. However, there are undesirable consequences of simply replacing these materials wi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d79cf557a102606ab760eabf7c8621f8
https://doi.org/10.1016/b978-0-12-802710-3.00012-x
https://doi.org/10.1016/b978-0-12-802710-3.00012-x