Using multigrid methods for the computation of reactive flows at low mach numbers

Author(s):  
Sébastien Paxion ◽  
Dominique Thévenin ◽  
Peter Bastian ◽  
Sébastien Candel
2001 ◽  
pp. 393-398
Author(s):  
Sébastien Paxion ◽  
Dominique Thévenin ◽  
Achim Gordner ◽  
Romain Baron ◽  
Peter Bastian

2000 ◽  
Vol 129 (1-3) ◽  
pp. 267-274 ◽  
Author(s):  
Olga Filippova ◽  
Dieter Haenel

2010 ◽  
Vol 13 (6) ◽  
pp. 511-528 ◽  
Author(s):  
A. Yarahmadi ◽  
Reza Hosseini ◽  
M. R. H. Nobari

1998 ◽  
Author(s):  
Mark Busby ◽  
Pasquale Cinnella
Keyword(s):  

Author(s):  
V. S. IVANOV ◽  
◽  
V. S. AKSENOV ◽  
S. M. FROLOV ◽  
P. A. GUSEV ◽  
...  

Modern high-speed unmanned aerial vehicles are powered with small-size turbojets or ramjets. Existing ramjets operating on the thermodynamic cycle with de§agrative combustion of fuel at constant pressure are efficient at flight Mach numbers M ranging from about 2 to 6.


1989 ◽  
Author(s):  
A. A. Amsden ◽  
P. J. O'Rourke ◽  
T. D. Butler

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