Boundary-layer and stalling characteristics of the NACA 63-009 airfoil section /
A wind-tunnel investigation was conducted to determine the boundary-layer and stalling characteristics of the NACA 63-009 airfoil section. The data obtained include pressure-distribution measurements, tuft studies, and boundary-layer measurements, particularly in the vicinity of the leading edge whe...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1949
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1894 |
| Subjects: |
Internet
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| Call Number: |
NACA TN 1894 |
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