Mach number and pressure measurements on afterbody of blunt-nose model in free flight at hypersonic speeds
Measurements of the Mach number and pressure on the afterbody of a blunt-nosed model in free flight at Mach numbers from 6.5 to 14
1960-04-01
Report
Keine Angabe
Englisch
Drag Reduction for Spike Attached to Blunt-Nosed Body at Mach 6
Online Contents | 2010
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