Fully corrected results for airfoils presented in useful range of shapes; with data so made available, airplane designer may intelligently choose best possible airfoil section for given application and may predict to reasonable degree aerodynamic characteristics to be expected in flight from section shape chosen.
Tests of related forward-camber airfoils in variable-density wind tunnel
Nat Advisory Committee Aeronautics -- Report
35 pages
Bibliography
Report
English
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Tests of related forward-camber airfoils in variable density wind tunnel
Engineering Index Backfile | 1937
|Tests of related forward-camber airfoils in variable density wind tunnel
Engineering Index Backfile | 1937
|Engineering Index Backfile | 1935
|