Wind-tunnel investigation and analysis of the effects of end plates on the aerodynamic characteristics of an unswept wing /
Wind-tunnel results on end-plate effects on the aerodynamic characteristics of an unswept and untapered wing of aspect ratio 4 are presented, and experimental values of the end-plate effects on the lift-curve slope and induced drag are determined and compared with theory. Expressions are developed f...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1951
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2440 |
| Subjects: |
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 2440 |
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