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Effect of design features on performance of a double-annular ram-induction combustorAn extensive test program was undertaken to determine the effect of many design features such as the size and number of air scoops, and the type of diffuser airflow distribution to use to optimize performance of a double-annular ram-induction combustor of 94 cm outer diameter. Six combustor configurations were tested. It was found that a snouted double annular combustor built with 256 ram-induction air scoops with a combustor open area giving a total pressure loss of 5.0 percent at a diffuser inlet Mach number of 0.25 gave the best overall performance of the configurations tested.
Document ID
19750020000
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Schultz, D. F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1975
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-8210
NASA-TN-D-7878
Report Number: E-8210
Report Number: NASA-TN-D-7878
Accession Number
75N28072
Funding Number(s)
PROJECT: RTOP 505-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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