FlightGlobal.com
Home
Premium
Archive
Video
Images
Forum
Atlas
Blogs
Jobs
Shop
RSS
Email Newsletters
You are in:
Home
Aviation History
1951
1951 - 1318.PDF
PLIGHT, lijuly 195* ARMSTRONG SIDDELEY GAS TURBINE DEVELOPMENT small frontal area is one result of the annular combustion chamber thrust per unit of frontal area =95 per sq Armktro WER ERFORMAJNCE ALREADY 7J COVENTRY •G SIDJELEY MOTCRS LIMITED, awker S iddeley CroupARMSTRO*
Sign up to
Flight Digital Magazine
Flight Print Magazine
Airline Business Magazine
E-newsletters
RSS
Events
