Investigation of an approximately 0.178-chord-thick NACA 6-series-type airfoil section equipped with sealed internally balanced 0.20-chord ailerons and with a 0.05-chord tab / Fioravante Visconti.
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| Main Author: | |
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| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1948.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1590. |
| Subjects: |
PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/1590
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| Y 3.N 21/5:6/1590 | Available Place a Hold |