Effect of taper ratio on the low-speed rolling stability derivatives of swept and unswept wings of aspect ratio 2.61 / Jack D. Brewer and Lewis R. FIsher.
Results of tests conducted in the 6-foot diameter rolling-flow test section of the Langley stability tunnel to determine the effects of varying taper ratio on the rolling and static stability characteristics of a swept wing are presented; results are also given for the effects of varying taper on an...
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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) ;
2555. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2555
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| Y 3.N 21/5:6/2555 | Available Place a Hold |