Experimental investigation of the effect of vertical-tail size and length and of fuselage shape and length on the static lateral stability characteristics of a model with 45 degree sweptback wing and tail surfaces / M.J. Queijo and Walter D. Wolhart.
Results are presented of an investigation made to determine the effects of vertical-tail size and length and of fuselage shape and length on the lateral-static-stability derivatives of a midwing airplane model with 45 degree sweptback wing and tail surfaces. Interference between the various model co...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1950.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2168. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2168
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| Y 3.N 21/5:6/2168 | Available Place a Hold |