Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Matthew C. Billingsley"'
Publikováno v:
Analytical and Bioanalytical Chemistry. 415:2411-2423
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::69b4c2dba819ac0123288d2773ad863e
https://doi.org/10.1007/s00216-022-04348-1
https://doi.org/10.1007/s00216-022-04348-1
Publikováno v:
Analytical and bioanalytical chemistry.
Tile-based Fisher ratio (F-ratio) analysis of comprehensive two-dimensional gas chromatography time-of-flight mass spectrometry (GC × GC-TOFMS) data is a powerful, supervised discovery methodology for pinpointing sample class-distinguishing analytes
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=pmid________::a7253b12d8af0507036bf0d7e65165aa
https://pubmed.ncbi.nlm.nih.gov/36181512
https://pubmed.ncbi.nlm.nih.gov/36181512
Autor:
Matthew C. Billingsley, Mark A. McHugh, Babatunde A. Bamgbade, Robert M. Enick, Hseen O. Baled, Rajendar R. Mallepally
Publikováno v:
Journal of Chemical & Engineering Data. 65:3221-3229
Rocket propellants are subjected to extreme thermodynamic conditions in high-performance liquid rocket engines, with temperatures in excess of 700 K and pressures nearing 100 MPa. Knowledge of the ...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aba7419cd5327e0690a4036a9f6277ab
https://doi.org/10.1021/acs.jced.0c00220
https://doi.org/10.1021/acs.jced.0c00220
Publikováno v:
Energy & Fuels. 34:4084-4094
Increasingly stringent requirements for aerospace propulsion system performance, reliability, and operability motivate quantitative connections between fuel composition, physical characteristics, and system performance. Chemically accurate assessment
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b6b492f5d4825d965724473ff29de89f
https://doi.org/10.1021/acs.energyfuels.9b04108
https://doi.org/10.1021/acs.energyfuels.9b04108
Autor:
Babatunde A. Bamgbade, Robert M. Enick, Matthew C. Billingsley, Mark A. McHugh, Rajendar R. Mallepally, Hseen O. Baled
Publikováno v:
Fuel. 253:1193-1203
Liquid rocket propellants are subject to wide ranges of temperature and pressure when flowing through high performance liquid rocket engines. For example, as rocket propellant (RP) is used for regenerative cooling, near-wall fluid temperatures can ex
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c3ad56f0d32440dc3b1faddd10501d62
https://doi.org/10.1016/j.fuel.2019.05.089
https://doi.org/10.1016/j.fuel.2019.05.089
Autor:
Carlos G. Fraga, Matthew C. Billingsley, Benjamin Kehimkar, Robert E. Synovec, Thomas J. Bruno, Jamin C. Hoggard, Luke C. Marney
Publikováno v:
Journal of Chromatography A. 1327:132-140
There is an increased need to more fully assess and control the composition of kerosene-based rocket propulsion fuels such as RP-1. In particular, it is critical to make better quantitative connections among the following three attributes: fuel perfo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7b8b1d389738c1ff3e2400216398d6fb
https://doi.org/10.1016/j.chroma.2013.12.060
https://doi.org/10.1016/j.chroma.2013.12.060
Publikováno v:
Talanta. 153
The chemical composition and several physical properties of RP-1 fuels were studied using comprehensive two-dimensional (2D) gas chromatography (GC×GC) coupled with flame ionization detection (FID). A “reversed column” GC×GC configuration was i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::dd3565cd34dc64aca3395caf20e2e2dc
https://pubmed.ncbi.nlm.nih.gov/27130110
https://pubmed.ncbi.nlm.nih.gov/27130110
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
A model is developed of the steady three-dimensional combined flow of fluid, heat and electricity in an experimental apparatus designed to test fuel thermal stability. A numerical simulation is performed for the purposes of model validation and asses
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::df3d03f0aba0105525e3a3f0f5b29552
https://doi.org/10.2514/6.2015-4212
https://doi.org/10.2514/6.2015-4212
Autor:
Matthew C. Billingsley, Robert E. Synovec, Benjamin Kehimkar, Thomas J. Bruno, Brendon A. Parsons, Jamin C. Hoggard
Publikováno v:
Analytical and bioanalytical chemistry. 407(1)
Recent efforts in predicting rocket propulsion (RP-1) fuel performance through modeling put greater emphasis on obtaining detailed and accurate fuel properties, as well as elucidating the relationships between fuel compositions and their properties.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c06b7193f4039e434475a191960e4c98
https://pubmed.ncbi.nlm.nih.gov/25315453
https://pubmed.ncbi.nlm.nih.gov/25315453
Autor:
Matthew C. Billingsley
Publikováno v:
44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
In an effort to enable reusable, high-performing liquid rocket engines, a comprehensive experimental and numerical investigation of the thermal performance (thermal stability and heat transfer characteristics) of RP-2 is underway at the Air Force Res
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3561032b261868528a44a3bcfa72d8c1
https://doi.org/10.2514/6.2008-5126
https://doi.org/10.2514/6.2008-5126