Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift
1950-08-11
Miscellaneous
No indication
English
Drag Force Balance of a Blunt and Divergent Trailing-Edge Airfoil
Online Contents | 2010
|Analysis of Blunt Trailing Edge Airfoils
AIAA | 2003
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