Hydrodynamic and aerodynamic tests of a family of models of seaplane floats with varying angles of dead rise N.A.C.A. models 57-A, 57-B, and 57-C /
Three models of v-bottom floats for twin-float seaplanes (N.A.C.A. models 57-A, 57-B, and 57-C) having angles of dead rise of 20 dgrees, 25 degrees, and 30 degrees, respectively, were tested in the N.A.C.A. tank and in the N.A.C.A. 7- by 10-foot wind tunnel. Within the range investigated, the effect...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington D.C. :
National Advisory Committee for Aeronautics,
1939
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
716 |
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Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Stanford University
| Call Number: |
ISIL:US-CST NACA TN 716 |
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