A simplified mathematical model for calculating aerodynamic loading and downwash for wing-fuselage combinations with wings / Martin Zlotnick and Samuel W. Robinson, Jr.
For the purpose of calculating the aerodynamic loading on the fuselage, the midwing wing-fuselage combination with a fuselage of circular cross section can be represented by a simple system of horseshoe vortices located on the wing with images located inside the fuselage. By using this simplified ma...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1954.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3057. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3057
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| Y 3.N 21/5:6/3057 | Available Place a Hold |