Effects of modifications to the leading-edge region on the stalling characteristics of the NACA 63₁-012 airfoil section / John A. Kelly.
A wind-tunnel investigation was conducted to determine the stalling characteristics of the NACA 63₁-012 airfoil section with various modifications to the leading edge region. The modifications consisted of alterations to the basic contour and addition of a leading-edge flap. The data presented were...
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| Main Author: | |
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1950.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2228. |
| Subjects: |
PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2228
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| Y 3.N 21/5:6/2228 | Available Place a Hold |