model aircraft
Pages
(Move to ...)
HOME
AERO PROJECTS
AERO MODELLING VIDEOS
TUTORIALS
AVIATION JOBS
▼
Sunday, May 13, 2012
Thrust distribution Combustion chambers
Combustion chambers
14. The conditions at the combustion chamber inlet are the same as the conditions at the diffuser outlet, i.e. 21,235 lb. Therefore, given that the combustion chamber-
No comments:
Post a Comment
‹
›
Home
View web version
No comments:
Post a Comment