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Applications of Modern Hydrodynamics to Aeronautics. Part 1: Fundamental Concepts and the Most Important Theorems. Part 2: ApplicationsA discussion of the principles of hydrodynamics of nonviscous fluids in the case of motion of solid bodies in a fluid is presented. Formulae are derived to demonstrate the transition from the fluid surface to a corresponding 'control surface'. The external forces are compounded of the fluid pressures on the control surface and the forces which are exercised on the fluid by any solid bodies which may be inside of the control surfaces. Illustrations of these formulae as applied to the acquisition of transformations from a known simple flow to new types of flow for other boundaries are given. Theoretical and experimental investigations of models of airship bodies are presented.
Document ID
19800006775
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Report
Authors
Prandtl, L.
(National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Date Acquired
August 10, 2013
Publication Date
December 1, 1979
Publication Information
Publication: NASA. Ames Res. Center Classical Aerodyn. Theory
Subject Category
Aerodynamics
Report/Patent Number
NACA-TR-116
Accession Number
80N15034
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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