Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90720/1/AIAA-2011-6125-190.pd
An advanced engineering computational model has been developed to aid in the analysis of chemical ro...
Although a lot of research and development has been done to understand and master the major physics ...
In this work an efficient numerical framework for the prediction of wall heat loads in Liquid Rocket...
A LES combustion model for the prediction of wall-heat transfer in rocket engines and confined combu...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97098/1/AIAA2012-3744.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83652/1/AIAA-2010-1525-645.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76294/1/AIAA-2007-5592-693.pd
A three-dimensional computational model of an experimental rectangular combustion chamber was develo...
Complexities of liquid rocket engine heat transfer which involve the injector faceplate and film coo...
Reacting flow and thermal fields around the injector critically affect the performance and life of l...
Reacting flow and thermal fields around the injector critically affect the performance and life of l...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76814/1/AIAA-2009-449-927.pd
This paper puts forth the case for the need for improved injector design tools to meet NASA s Vision...
A priori prediction of rocket engine combustor flowfields is extremely difficult due to a number of ...
Processing data on heat flux and chemical composition in rocket combustion chamber boundary flow - t...
An advanced engineering computational model has been developed to aid in the analysis of chemical ro...
Although a lot of research and development has been done to understand and master the major physics ...
In this work an efficient numerical framework for the prediction of wall heat loads in Liquid Rocket...
A LES combustion model for the prediction of wall-heat transfer in rocket engines and confined combu...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97098/1/AIAA2012-3744.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83652/1/AIAA-2010-1525-645.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76294/1/AIAA-2007-5592-693.pd
A three-dimensional computational model of an experimental rectangular combustion chamber was develo...
Complexities of liquid rocket engine heat transfer which involve the injector faceplate and film coo...
Reacting flow and thermal fields around the injector critically affect the performance and life of l...
Reacting flow and thermal fields around the injector critically affect the performance and life of l...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76814/1/AIAA-2009-449-927.pd
This paper puts forth the case for the need for improved injector design tools to meet NASA s Vision...
A priori prediction of rocket engine combustor flowfields is extremely difficult due to a number of ...
Processing data on heat flux and chemical composition in rocket combustion chamber boundary flow - t...
An advanced engineering computational model has been developed to aid in the analysis of chemical ro...
Although a lot of research and development has been done to understand and master the major physics ...
In this work an efficient numerical framework for the prediction of wall heat loads in Liquid Rocket...
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