Design and analysis of Gas Turbine Multi Linear Combustion Chamber
Stage 1: Completed on 31 Dec 2015 Stage 2: Completed on 18 Jan 2016
Top 15 Projects have been shortlisted for Stage 3. Stage 3: Experts from our team will be guiding the teams in completing their projects. This stage ends on 31 March 2016. Stage 4: Announcement of prizes on 15 April 2016
Outcome: High thrust and fuel efficiency Description: By using multy linear combustion chamber we can improve combustion chamber efficiency and thrust production and we can provide efficient cooling system for the combustion chamber
