Supersonic Two-Dimensional Minimum Length Nozzle Design at High Temperature. Application for Air

When the stagnation temperature of a perfect gas increases, the specific heat ratio does not remain constant any more, and start to vary with this temperature. The gas remains perfect, its state equation remains always valid, except it will name in more calorically imperfect gas or gas at High Tempe...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Chinese journal of aeronautics 2007-02, Vol.20 (1), p.29-39
Hauptverfasser:	Toufik, Zebbiche, ZineEddine, Youbi
Format:	Artikel
Sprache:	eng
Schlagworte:	calorically imperfect gas conception interpolation method of characteristics minimum length nozzle Prandtl Meyer function Simpson quadrature stretching function supersonic flow supersonic parameters
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!