Aerodynamics of the fuselage /

The present report deals with a number of problems, particularly with the interaction of the fuselage with the wing and tail, on the basis of simple calculating method's derived from greatly idealized concepts. For the fuselage alone it affords, in variance with potential theory, a certain fric...

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Bibliographic Details
Main Author: Multhopp, H
Corporate Author: United States National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1942]
Series:Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 1036
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Stanford University

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Call Number: NACA TM 1036