scholarly journals Hydrodynamic forces acting on a cylinder in motion, and the idea of a "hydrodynamic centre."

There are two general methods of determining the forces acting on a cylinder due to the two-dimensional motion of a surrounding liquid. One is applicable to the case of a stationary cylinder in a stream, in the form X - Y = 1/2 p ∫( dw / dz ) 2 dz . (1.1) M = -1/2 pR ∫( dw / dz ) 2 z . dz (1.2) where X and Y are the components of the resultant force, parallel to the x and y axes, and M is its moment about tbs origin; p is the density of the fluid, and w is the velocity potential-stream-function for the fluid motion; z is as usual the complex variable x + y . The other is that obtained from the general theory of the "impulse. The first of these is unable to deal with a rotating cylinder, and the second is unable to include "circulation." In the course of an investigation of the effects of rotation upon the circulation round, and the forces acting upon, a Joukowski aerofoil, to which problem neither method applies, since the combined effect of rotation and circulation is needed, a quite general result was obtained, which it is thought worth while to publish separately.

1. The problem of any barrier in a fluid stream is best attacked by the method due to Levi-Civita, of which useful accounts, with extensions, are given by Cisotti and Brillouin. The resultant pressure for any barrier has been given in terms of the constants defining the barrier; but the calculations required to find the line of action of this pressure have not been carried out. It is our object to supply this deficiency here. The motion is two-dimensional. Let the complex variable z (≡ x + iy ) define position in any plane perpendicular to the generators of the barrier, the x axis being parallel to the direction of the stream at infinity. We define u = ∂ϕ/∂ x = ∂ψ/∂ y , v = ∂ϕ/∂ y = -∂ψ/∂ x , where u , v are the velocity components, and ϕ, ψ are the velocity potential and stream function respectively. Let w ≡ ϕ + iψ and define ζ, Ω, r, θ so that ζ ≡ re θ = dz / dw ; Ω = log ζ ≡ log r + iθ . (1)


1. In the previous papers of this series (Morris 1937, 1938; referred to subsequently as “I” and “II”) I have developed a general expression for the velocity potential of the two-dimensional fluid motion surrounding an infinite cylinder of general shape, moving in any manner perpendicular to its axis, in inviscid and incompressible fluid. From this expression I derived in “I” the kinetic energy of the fluid when the circulation is zero and in the more general case the forces and couple on the cylinder, including also in “II” the effect of a trail of vortices extending downstream from an assumed trailing edge at the rear of the cylinder. In a brief discussion at the end of “II” the general formulae obtained were reduced for the case of an aerofoil of small thickness and small symmetrical camber, but using the particular hydrodynamical assumptions made by Wagner in his theory of accelerated motions; according to which the circulation associated with the trail is just sufficient to cancel the general circulation round the aerofoil. This was done in order to obtain comparison with the only previous attempt to calculate the effects of rotation and acceleration.


(1) It is not so long ago that it was generally believed that the "classical" hydrodynamics, as dealing with perfect fluids, was, by reason of the very limitations implied in the term "perfect," incapable of explaining many of the observed facts of fluid motion. The paradox of d'Alembert, that a solid moving through a liquid with constant velocity experienced no resultant force, was in direct contradiction with the observed facts, and, among other things, made the lift on an aeroplane wing as difficult to explain as the drag. The work of Lanchester and Prandtl, however, showed that lift could be explained if there was "circulation" round the aerofoil. Of course, in a truly perfect fluid, this circulation could not be produced—it does need viscosity to originate it—but once produced, the lift follows from the theory appropriate to perfect fluids. It has thus been found possible to explain and calculate lift by means of the classical theory, viscosity only playing a significant part in the close neighbourhood ("grenzchicht") of the solid. It is proposed to show, in the present paper, how the presence of vortices in the fluid may cause a force to act on the solid, with a component in the line of motion, and so, at least partially, explain drag. It has long been realised that a body moving through a fluid sets up a train of eddies. The formation of these needs a supply of energy, ultimately dissipated by viscosity, which qualitatively explains the resistance experienced by the solid. It will be shown that the effect of these eddies is not confined to the moment of their birth, but that, so long as they exist, the resultant of the pressure on the solid does not vanish. This idea is not absolutely new; it appears in a recent paper by W. Müller. Müller uses some results due to M. Lagally, who calculates the resultant force on an immersed solid for a general fluid motion. The result, as far as it concerns vortices, contains their velocities relative to the solid. Despite this, the term — ½ ρq 2 only was used in the pressure equation, although the other term, ρ ∂Φ / ∂t , must exist on account of the motion. (There is, by Lagally's formulæ, no force without relative motion.) The analysis in the present paper was undertaken partly to supply this omission and partly to check the result of some work upon two-dimensional potential problems in general that it is hoped to publish shortly.


2008 ◽  
Vol 144 (3) ◽  
pp. 673-688 ◽  
Author(s):  
Francisco Javier Gallego ◽  
Miguel González ◽  
Bangere P. Purnaprajna

AbstractIn this paper we prove that most ropes of arbitrary multiplicity supported on smooth curves can be smoothed. By a rope being smoothable we mean that the rope is the flat limit of a family of smooth, irreducible curves. To construct a smoothing, we connect, on the one hand, deformations of a finite morphism to projective space and, on the other hand, morphisms from a rope to projective space. We also prove a general result of independent interest, namely that finite covers onto smooth irreducible curves embedded in projective space can be deformed to a family of 1:1 maps. We apply our general theory to prove the smoothing of ropes of multiplicity 3 on P1. Even though this paper focuses on ropes of dimension 1, our method yields a general approach to deal with the smoothing of ropes of higher dimension.


Author(s):  
D. Porter

AbstractThe two-dimensional configuration is considered of a fixed, semi-infinite, vertical barrier extending downwards from a fluid surface and having, at some depth, a gap of arbitrary width. A train of surface waves, incident on the barrier, is partly transmitted and partly reflected. The velocity potential of the resulting fluid motion is determined by a reduction procedure and also by an integral equation formulation. It is shown that the two methods lead to the same Riemann–Hilbert problem. Transmission and reflexion coefficients are calculated for several values of the ratio gap width/mean gap depth.


1952 ◽  
Vol 19 (4) ◽  
pp. 537-542
Author(s):  
Yi-Yuan Yu

Abstract Gravitational stresses around a horizontal tunnel opening are determined by means of Muschelišvili’s complex variable method for solving two-dimensional elasticity problems. The tunnel is located at a large but finite depth underneath the horizontal ground surface. It has the shape of a general ovaloid, including the rounded-cornered square, the ellipse, and the circle as its special cases. The surrounding material is assumed to be elastic, isotropic, and homogeneous. Two problems are solved. In one problem an unlined tunnel is considered, which has a boundary free from external stresses. In the other the tunnel has a rigid lining, and a perfect bond is assumed to exist between the lining and the surrounding material so that the displacements at the boundary are zero.


1. Calculations of wave resistance, corresponding to a pressure system travelling over the surface, have hitherto been limited to two-dimensional fluid motion; in those cases, the distribution of pressure on the surface is one-dimensional, and the regular waves produced have straight, parallel crests. The object of the following paper is to work out some cases when the surface pressure is two-dimensional and the wave pattern is like that produced by a ship. A certain pressure system symmetrical about a point is first examined, and more general distributions are obtained by superposition. By combining two simple systems of equal magnitude, one in rear of the other, we obtain results which show interesting interference effects. In similar calculations with line pressure systems, at certain speeds the waves due to one system cancel out those due to the other, and the wave resistance is zero; the corresponding ideal form of ship has been called a wave-free pontoon. Such cases of perfect interference do not occur in three-dimensional problems; the graph showing the variation of wave resistance with velocity has the humps and hollows which are characteristic of the resistance curves of ship models. Although the main object is to show how to calculate the wave resistance for assigned surface pressures of considerable generality, it is of interest to interpret some of the results in terms of a certain related problem. With certain limitations, the waves produced by a travelling surface pressure are such as would be caused by a submerged body of suitable form. The expression for the wave resistance of a submerged sphere, given in a previous paper, is confirmed by the following analysis. It is also shown how to extend the method to a submerged body whose form is derived from stream lines obtained by combining sources and siuks with a uniform stream; in particular, an expression is given for the wave resistance of a prolate spheroid moving in the direction of its axis.


2004 ◽  
Vol 126 (6) ◽  
pp. 963-984 ◽  
Author(s):  
Nadeem Hasan ◽  
Sanjeev Sanghi

The present study involves a numerical investigation of buoyancy induced two-dimensional fluid motion in a horizontal, circular, steadily rotating cylinder whose wall is subjected to a periodic distribution of temperature. The axis of rotation is perpendicular to gravity. The governing equations of mass, momentum and energy, for a frame rotating with the enclosure, subject to Boussinesq approximation, have been solved using the Finite Difference Method on a Cartesian colocated grid utilizing a semi-implicit pressure correction approach. The problem is characterized by four dimensionless parameters: (1) Gravitational Rayleigh number Rag; (2) Rotational Rayleigh number RaΩ; (3) Taylor number Ta; and (4) Prandtl number Pr. The investigations have been carried out for a fixed Pr=0.71 and a fixed Rag=105 while RaΩ is varied from 102 to 107. From the practical point of view, RaΩ and Ta are not independent for a given fluid and size of the enclosure. Thus they are varied simultaneously. Further, an observer attached to the rotating cylinder, is stationary while the “g” vector rotates resulting in profound changes in the flow structure and even the flow direction at low enough flow rates RaΩ<105 with phase “ϕg” of the “g” vector. For RaΩ⩾105, the global spatial structure of the flow is characterized by two counter-rotating rolls in the rotating frame while the flow structure does not alter significantly with the phase of the rotating “g” vector. The frequency of oscillation of Nusselt number over the heated portion of the cylinder wall is found to be very close to the rotation frequency of the cylinder for RaΩ⩽105 whereas multiple frequencies are found to exist for RaΩ>105. The time mean Nusselt number for the heated portion of the wall undergoes a nonmonotonic variation with RaΩ, depending upon the relative magnitudes of the different body forces involved.


2002 ◽  
Vol 04 (03) ◽  
pp. 213-236 ◽  
Author(s):  
OSAMU KATAI ◽  
KENTARO TODA ◽  
HIROSHI KAWAKAMI

Focusing on the interaction among members' attitudes toward issues of common concern and members' expectance toward other members' attitudes, type classification of societal conflicts and their degree of strength are clarified. For the purpose, a vigorous theoretical framework for the examination of interrelationships among various normative concepts such as obligation, permission, prohibition, etc. is introduced, on the basis of the general theory on norms, deontic logic. By presuming several plausible laws on the way of the resolution of these conflicts and by introducing a two-dimensional representation of the conflicts with one axis representing the degree of imbalance and the other axis representing the cohesiveness of systems, a characterization method of conflict resolution processes is obtained, through which prediction and analysis of actual resolution processes can be done.


1988 ◽  
Vol 1 (21) ◽  
pp. 45
Author(s):  
Mark Cooker ◽  
Howell Peregrine

A method is described for the computation of the two-dimensional unsteady motion of a solitary wave passing over submerged breakwaters. Far from the breakwater the fluid is assumed static and the sea bed is level. The fluid motion is assumed to be irrotational, incompressible and inviscid. The exact boundary conditions at the free surface and the impermeable bed are satisfied. Laplace's equation for the velocity potential is solved using a boundary integral method. Numerical results are reported which show the variety of ways in which solitary waves are distorted when they encounter submerged breakwaters.


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