Primitive-variable model applications to solid-fuel ramjet combustion

An adaptation of a primitive-variable finite-difference computer program was accomplished in order to predict the reacting flowfield in a solid-fuel ramjet. The study compares the predictions of the primitive-variable computer model with predictions of an earlier stream function-vorticity computer m...

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Veröffentlicht in:	Journal of spacecraft and rockets 1981-01, Vol.18 (1), p.89-94
Hauptverfasser:	Stevenson, Charles A, Netzer, David W
Format:	Artikel
Sprache:	eng
Schlagworte:	Solid fuels
Online-Zugang:	Volltext
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