SUPERSONIC AXISYMMETRIC NOZZLE DESIGN BY MASS FLOW TECHNIQUES UTILIZING A DIGITAL COMPUTER

This report presents a method to design the inviscid wall contour of a supersonic, axisymmetric nozzle producing uniform parallel flow at the exit. The calculation methods used are restricted to a perfect gas. The axis velocity distribution must be specified. A complete flow pattern within the nozzl...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Moger, W C, Ramsay, D B
Format:	Report
Sprache:	eng
Schlagworte:	AXISYMMETRIC FLOW COMPUTER PROGRAMMING Computer Programming and Software DIFFERENTIAL EQUATIONS DIGITAL COMPUTERS Fluid Mechanics GAS FLOW METHOD OF CHARACTERISTICS NOZZLES NUMERICAL INTEGRATION SUPERSONIC FLOW SUPERSONIC NOZZLES TRANSPORT PROPERTIES
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!