Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds / Thomas R. Turner.
An investigation at transonic speeds has been made in the Langley high-speed 7- by 10-foot tunnel to determine the effect of wing sweep on the maximum-lift characteristics of a series of wings having aspect ratio of 4, taper ratio of 0.6, and NACA 65A006 airfoil sections. The Mach number varied from...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1955.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3468. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3468
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| Y 3.N 21/5:6/3468 | Available Place a Hold |