Effects of wing position and fuselage size on the low-speed static and rolling stability characteristics of a delta-wing model / Alex Goodman and David F. Thomas, Jr.
An investigation was made to determine the effects of wing position and fuselage size on the low-speed static and rolling stability characterististics of airplane models having a triangular wing and vertical tail surfaces.
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| Other title: | Technical report archive and image library. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1954.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3063. |
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Internet
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| Call Number: |
Y 3.N 21/5:6/3063
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| Y 3.N 21/5:6/3063 | Available Place a Hold |