Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes /

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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Bibliographic Details
Main Author: Riebe, John M
Corporate Author: United States National Advisory Committee for Aeronautics
Other Authors: Naeseth, Rodger L
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1952
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 2489
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Stanford University

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Call Number: NACA TN 2489