Cocks, PAT and Dawes, WN and Cant, RS (2012) Simulations of the SCHOLAR scramjet experiment. In: UNSPECIFIED.Full text not available from this repository.
The DDES method is employed to investigate the complex physics involved in supersonic combustion and in particular in the SCHOLAR scramjet test case. The influence on computational results of prescribing turbulent fluctuations at the entrance to the combustion chamber is investigated. The interaction of shock waves, vortices, turbulence and combustion is studied and the existence of secondary vortices on the upper will of the combustor is proposed. © 2012 by Peter Cocks.
|Item Type:||Conference or Workshop Item (UNSPECIFIED)|
|Divisions:||Div A > Turbomachinery|
Div A > Energy
|Depositing User:||Cron Job|
|Date Deposited:||18 May 2016 19:23|
|Last Modified:||26 May 2016 23:41|