Wind-tunnel investigation of the effect of power and flaps on the static longitudinal stability characteristics of a single-engine low-wing airplane model /
As part of a comprehensive investigation of the effect of power, flaps, and wing position on static stability, tests were made in the Langley 7- by 10-foot tunnel to determine the longitudinal stability of characteristics with and without power of a typical low-wing, single-engine airplane model wit...
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| Other Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington D.C. :
National Advisory Committee for Aeronautics,
1947
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1239 |
| Subjects: | |
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| Call Number: |
ISIL:US-CST NACA TN 1239 |
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