Effect of axisymmetric sonic nozzle geometry on characteristics of supersonic air jet

Journal of Thermal Science

Volumn 13, Issue 2, 2004, Pages 121-126

  Matsuo, Shigeru ^a   Tanaka, Masanori ^a   Otobe, Yumiko ^b   Kashimura, Hideo ^b   Kim, Heuy Dong ^c   Setoguchi, Toshiaki ^a  

^a SAGA UNIVERSITY   (Japan)

^b KITAKYUSHU NATIONAL COLLEGE OF TECHNOLOGY   (Japan)

^c Andong National University   (South Korea)

Author keywords

Compressible flow; Non equilibrium condensation; Simulation; Supersonic jet

Indexed keywords

COMPRESSIBLE FLOW; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; GEOMETRY; NOZZLES; ORIFICES;

NON EQUILIBRIUM CONDENSATION; SUPERSONIC JET;

SUPERSONIC AIRCRAFT;

EID: 4043092655     PISSN: 10032169     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11630-004-0019-2     Document Type: Article

References (14)

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