Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes / John M. Riebe and Rodger L. Naeseth.
An investigation was made in the Langley 300-mph 7- by 10-foot tunnel to determine the aerodynamic characteristics of a refined deep-step planing-tail hull with various forebody and afterbody shapes and, for comparison, a streamline body simulating the fuselage of a modern transport airplane. The re...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1952.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2489. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2489
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| Y 3.N 21/5:6/2489 | Available Place a Hold |