Stabilty and Transition Analysis of NEXST-1 NLF Wing Model at Mach 2
41st, Aerospace sciences meeting ; 2003 ; Reno, NV
2003-01-01
ALL
Paper nos AIAA-2003-0001 to AIAA-2003-1359 with gaps
Aufsatz (Konferenz)
Englisch
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CFD VALIDATION STUDY OF NEXST-1 NEAR MACH 1
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