Section characteristics of an NACA 0006 airfoil with area suction near the leading edge / James A. Weiberg and Robert E. Dannenberg.
An investigation has been made of the low-speed two-dimensional aerodynamic characteristics of an NACA 0006 airfoil with area suction near the leading edge. The maximum lift coefficient of the airfoil was increased from 0.87 to 1.25 for a section flow coefficient of 0.0010 at a free-stream velocity...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1954.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3285. National Advisory Committee for Aeronautics ; 3285. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3285
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| Y 3.N 21/5:6/3285 | Available Place a Hold |