NASA NTRS · 19670044389
A general method for determining optimum thrust nozzle contours for chemically reacting gas flows.
Abstract
Optimum thrust nozzle contours for chemically reacting gas flows, obtaining set of partial differential equations for gas dynamic properties
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Hoffman, J. D.. 1967-04-01. A general method for determining optimum thrust nozzle contours for chemically reacting gas flows.. https://ntrs.nasa.gov/citations/19670044389
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