Zobrazeno 1 - 5
of 5
pro vyhledávání: '"John E. Colbert"'
Publikováno v:
Petroleum Science and Technology. 24:1097-1113
To gain a more complete understanding of the relevance of laboratory testing to predict fuel stability in advanced jet engine designs, the Navy single tube reactor (STR) was employed to examine the impact of copper contamination on fuel oxidation at
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::56db18925f54fd63a4b74aa2ad38d1ce
https://doi.org/10.1081/lft-200048190
https://doi.org/10.1081/lft-200048190
Publikováno v:
Energy & Fuels. 18:490-496
The fuel systems in advanced aircraft will subject the fuel to more severe thermal stress and increased recirculation than in current designs. This work was undertaken as part of a study to determi...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f58117abc755fe23aadbfb222322b077
https://doi.org/10.1021/ef0301093
https://doi.org/10.1021/ef0301093
Autor:
L. Salvucci, S. G. Pande, R. E. Morris, Dennis R. Hardy, C. J. Nowack, R. A. Kamin, John E. Colbert
Publikováno v:
Energy & Fuels. 15:224-235
Thermal deposition, based on carbon burn off, was evaluated in two turbulent flow and one laminar flow test devices. The two turbulent flow test devices were the Navy Aviation Fuel Thermal Stability Simulator (NAFTSS), developed by Rolls Royce, UK, f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::66e5506e9831f06c595591cf3c185c80
https://doi.org/10.1021/ef000187f
https://doi.org/10.1021/ef000187f
Autor:
Clarence J. Nowack, John E. Colbert
NAVAIRSYSCOM has evaluated the individual benefits of 3 different thermal stability improving additives (TSIAs) in jet fuel using 2 separate, small-scale test devices - one laminar flow and the other turbulent. Both systems pump fuel at constant flow
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0bda05ed421bb322fb1ed59f84e2d89e
https://doi.org/10.21236/ada383363
https://doi.org/10.21236/ada383363
