Estimated Performance of Radial-Flow Exit Nozzles for Air in Chemical Equilibrium

The thrust, boundary-layer, and heat-transfer characteristics were computed for nozzles having radial flow in the divergent part. The working medium was air in chemical equilibrium, and the boundary layer was assumed to be all turbulent. Stagnation pressure was varied from 1 to 32 atmospheres, stagn...

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Bibliographische Detailangaben

Hauptverfasser:	Englert, Gerald W., Kochendorfer, Fred D.
Format:	Report
Sprache:	eng
Schlagworte:	Fluid Mechanics And Heat Transfer
Online-Zugang:	Volltext bestellen
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