Investigation of the drag of blunt-nosed bodies of revolution in free flight at Mach numbers from 0.6 to 2.3
1953-06-11
Sonstige
Keine Angabe
Englisch
Drag Reduction for Spike Attached to Blunt-Nosed Body at Mach 6
Online Contents | 2010
|Theoretical investigation of flow field about blunt-nosed bodies in supersonic flight
Engineering Index Backfile | 1958
|SHEAR LAYER FLOW INDUCED BY BLUNT-NOSED BODIES
AIAA | 1963
|Experiments with inclined blunt-nosed bodies at Mo=2.45
TIBKAT | 1959
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