NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The Navier-Stokes Stress Principle for Viscous FluidsThe Navier-Stokes stress principle is checked in the light of Maxwell's mechanism of friction and in connection herewith the possibility of another theorem is indicated. The Navier-Stokes stress principle is in general predicated upon the conception of the plastic body. Hence the process is a purely phenomenological one, which Newton himself followed with his special theorem for one-dimensional flows. It remained for Maxwell to discover the physical mechanism by which the shear inflow direction is developed: According to it, this shear is only 'fictitious' as it merely represents the substitute for a certain transport on macroscopic motion quantity, as conditioned by Brown's moiecular motion and the diffusion, respectively. It is clear that this mechanism is not bound to the special case of the one-dimensioilal flows, but holds for any flow as expression of the diffusion, by which a fluid differs sharply from a plastic body. If it is remembered, on the other hand, that the cause of the stresses on the plastic body lies in a certain cohesion of the molecules, it appears by no means self evident that this difference in the mechanism of friction between fluid and plastic body should not prevail in the stress principle as well, although it certainly is desirable in any case, at least subsequently, to establish the general theorem in the sense of Maxwell. Actually, a different theorem is suggested which, in contrast to that by Navier-Stokes, has the form of an unsymmetrical matrix. Without anticipating a final decision several reasons are advanced by way of a special flow which seem to affirm this new theorem. To make it clear that the problem involved here still awaits its final solution, is the real purpose behind the present article.
Document ID
20030064898
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Mohr, Ernst
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 1942
Publication Information
Publication: Luftfahrtforschung
Volume: 18
Issue: 9
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NACA-TM-1029
Report Number: NACA-TM-1029
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available