Design of a Mach-6 Quiet-flow Wind-Tunnel Nozzle Using thee^*^*N Method for Transition Estimation
36th, Aerospace sciences meeting ; 1998 ; Reno; NV
1998-01-01
ALL
Nos AIAA 98-0001 to 98-1069 with gaps held only
Aufsatz (Konferenz)
Englisch
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