Open AccessSupersonic Axisymmetric Minimum Length Nozzle Conception at High Temperature with Application for Air
Author(s) -
Toufik Zebbiche
Publication year - 2008
Publication title -
international journal of aeronautical and space sciences
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.292
H-Index - 20
eISSN - 2093-274X
pISSN - 2093-2480
DOI - 10.5139/ijass.2008.9.1.001
Subject(s) - stagnation temperature , nozzle , mach number , perfect gas , mechanics , supersonic speed , stagnation pressure , rotational symmetry , discharge coefficient , stagnation point , transonic , choked flow , dissociation (chemistry) , thermodynamics , physics , materials science , chemistry , heat transfer , aerodynamics