Tests on airship models in variable-density wind tunnel to determine drag coefficients at zero pitch, and effect of fins and cars and of flat and streamline protruberances located at various positions along hull; range of Reynolds Number from 1,300,000 to 33,000,000.
Drag of two streamline bodies as affected by protuberances and appendages
Nat Advisory Committee Aeronautics -- Report
1932
8 pages
Report
English
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Engineering Index Backfile | 1934
|Emerald Group Publishing | 1934
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