https://catalogue-scientifique.canada.ca/record=2159962~S6*frc
Rechercher Kahandawala, Moshan S; Rechercher Corera, Shehan A; Rechercher Sidhu, Sukh S; Rechercher Williams, Skip; Rechercher Carter, Campbell D
dayton univ oh dept of mechanical and aerospace engineering, 2006
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...
Publication gouvernementale