NASA NTRS · 20090006600
Stagnation point reverse flow combustor
Abstract
A method for combusting a combustible fuel includes providing a vessel having an opening near a proximate end and a closed distal end defining a combustion chamber. A combustible reactants mixture is presented into the combustion chamber. The combustible reactants mixture is ignited creating a flame and combustion products. The closed end of the combustion chamber is utilized for directing combustion products toward the opening of the combustion chamber creating a reverse flow of combustion products within the combustion chamber. The reverse flow of combustion products is intermixed with combustible reactants mixture to maintain the flame.
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Zinn, Ben T., Neumeier, Yedidia, Seitzman, Jerry M., Jagoda, Jechiel, Weksler, Yoav. 2008-09-16. Stagnation point reverse flow combustor. https://ntrs.nasa.gov/citations/20090006600
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