Flow Measurements Downstream of a Single Bleed Hole in a Subsonic, Turbulent Boundary Layer Using a New 5-Hole Pressure Probe
37th, Aerospace sciences meeting ; 1999 ; Reno; NV
01.01.1999
ALL
Nos 99-0001 to 99-1096 with gaps
Aufsatz (Konferenz)
Englisch
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