https://catalogue-scientifique.canada.ca/record=2157374~S6*frc
Rechercher Kahandawala, Moshan S; Rechercher Corera, Shehan A; Rechercher Williams, Skip; Rechercher Carter, Campbell D; Rechercher Sidhul, Sukh S
air force research lab wright-patterson afb oh propulsion directorate, 2005
A single pulse reflected shock tube was used to investigate iso-octane ignition over the temperature range of 900-1400 K at a pressure of 1 atm. To account for...
Publication gouvernementale