The aerodynamic aspect of wing-fuselage fillets /
Model tests prove the feasibility of enhancing the aerodynamic qualities of wing-fuselage fillets by appropriate design of fuselage and wing roots. Abrupt changes from maximum fuselage height to wing chord must be avoided and every longitudinal section of fuselage and wing roots must be so faired an...
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| Main Author: | |
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1935]
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| Series: | Technical memorandum (United States. National Advisory Committee for Aeronautics) ;
no. 764 |
| Subjects: | |
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| Call Number: |
ISIL:US-CST NACA TM 764 |
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