AIAA 2006-1382 Numerical Modeling of Scramjet Combustor Flow Field Using Unstructured Point Implicit Finite Volume Method
44th, Aerospace sciences meeting ; 2006 ; Reno, NV
Aerospace sciences meeting ; 16625-16634
2006-01-01
10 pages
VOL 22 of 24 VOLS
Aufsatz (Konferenz)
Englisch
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