Wind-tunnel investigation at low speed of effect of size and position of closed air ducts on static longitudinal and static lateral stability characteristics of unswept-midwing models having wings of aspect ratio 2, 4, and 6 / Byron M. Jaquet and James L. Williams.
An investigation was made at a Mach number of 0.13 in the Langley stability tunnel in order to determine the effects of closed wing-root air ducts (horizontal) on the static longitudinal and static lateral stability characteristics of unswept-midwing models having wings of aspect ratio 2, 4, and 6....
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
[1955]
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3481. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3481
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| Y 3.N 21/5:6/3481 | Available Place a Hold |