An Experimental investigation of the NACA 63₁-012 airfoil section with leading-edge and midchord suction slots /
Lift, drag, pitching-moment, pressure-distribution, and boundary-layer data are given for two different leading-edge slots operating in conjunction with the midchord slot
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1950
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2041 |
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Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Stanford University
| Call Number: |
NACA TN 2041 |
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