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B24825

LABORATORIUM. VOOR SCHEEPSH'VDROMECHANICA

I-SAIL DESIGN AND PANEL CALCULATION

by

ir.J.A. Keuning

ing.A. Verslui,s

Repottno. 702-p

January 1 986

Deift University of Technology

Ship Hydromechanics Laboratory

Mekelweg2 2628 CD DELFT

TheNetherlands

Phone 015 -786882

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## AR Till

### ill

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Contents

Abstract

introduction

The Design proces Panel definition Panel calculation Examples Future Development Acknowledgement References

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Abs tract

Sail design and panel calculation

In this paper a method, developed at the Deift University of Technology, is described to calculate the panels of a sail of a

given geometry and: shape.

First the countours: of the sail are determined and presented.as three dimensional curves, the leech,, the luff and the foot of the

sail. Subsequently a number of cross-section shapes at different heights along the sail with prescribed camber and distribution of

camber along the cordline are selected.

With these data the computer:prog.ram calculates a. comlete three

dimensional polynomal representation of the sail and visualises the sail from different angles of view for the designer on a plot or visual display unit. In this way the designer may evaluate the

sail form and change it if necessarry.

If the designed sail is considered to be in accor6ance with the shape wanted, the designer places the panels over the sail in the way he feels most adequate for handling stresses and distortion of the sail in use, simply by specifying the ends of the seams of each panel. The computerprogram now calculates the shape of each seam in the sail as a three dimensional curve and calculates the offsets of the panels with the aid of a method used to calculate

the shape of developable surfaces.

The output of the program is presented.in such.a way that the pa-nels either can be plottted by hand or, if possibly, with the aid

of a numerically controled cutting machine.

In the paper various results of the program are presented as well

as some of the experience gained over the years by. using this

method both on the design-proces as on the construction of the

sails. Advantages and shortommings are outlined.

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1. Introduction

In this paper a method is described to design a sail and to

calcu-late the shape of the panels.

The initial work on this project started as early as 1976 with a

design and calculation procedure for genoas, using traditional

pa-nel layout. Much of this work has been kept restricted for use by the participants in the project only, i.e. the Delft University of TechnolOgy and Gaastra Sails. Later on this project has evolved to an all-round and versatile design and production method for all

kinds of sails, the final version of which is flow reported in this paper.

lJntill a decade or so the art of sailmaking was largely based on experience and intuition. This experience was gained using a trial

and error technique: by cutting the sails, examining the actual product afloat and correcting it when and where necessarry. The experience thus gained made it possible to construct sails without major faults but predicting the actual shape was hard to

be done and progress was slow.

In the last decade a tremendous change in the sailmaking art has occurred due to the availability of new materials and the pressure from the users to find new and even faster shapes in sails with less overall weight.

Detailed theoretical calculations of the optimal shapes for sails

will not be available for many years to come,. so these will have

to be found in practice. A valuable toolfor:optimising.the shape of sails is a possibility to cut the sails in such a way that the

shape designed on the drawing board is actually there:in the sail.

Sails will no longer be defined by the amount of broadseaming on different locations in the sail, thus leaving the actual shape

un-known, but by. specifying the amount and position of camber and

twist all over the span of the sail and leaving it to the computer to calculate the shape of the panels tO generate that specificly

defined sail.

By knowing that a given shape is in the actually build sail it is possible to compare the merits of each shape and by doing so to

find the optinium sail.

Also difficulties encountered by traditional sailmaking in

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fying the shape of the panels when completely new panel layouts must be used, as is nowadays common practice by the advent of

high-tech materials and the search for lighter and stronger sails, may easily be overcome by using this new technique. Any sailshape can be made by proper shaping Of the individual panels it is made of. One of the restrictions of the method is that the shape of the panels of the sails are being calculated as if they were

developa-ble surfaces. A developadevelopa-ble surface is one which may be unrolled

into a plane without distortion,. In practical terms this means

that only the four sides of each panel may be any kind of curved line but no cross-seams perpendicular to the side of the panel may be used. Cones and cilinders are known examples of developable

surfaces.

Traditionally thesekind of panels are used when making.a sail, except perhaps in the foot of mainsails, so this restriction poses

no real problems. When planning the. panel layout. carefull

conside-ration must be given to this limitation so that no "unbuildable"

sails are designed.

A second limitation of the present procedure is that no account has been taken of distortion of the sail due to the loading on the

sail in actual use. Some of the distortion may be accounted for in the design procedure, by making for instance a less full sail with

little or no twist, and the camber positioned a little more forward,

but furthermore this assumption must be jUstified by using strong and stretch resistant new materials. However a large number of

test sails have been made using regular Dacron and this yielded very good results. Deformation of the sail under load was dealt with in practice using sheet and hailyard tension just as usual, but much less of all this was necessarry to keep the optimum shape.

Since the shape of the panels is completely defined itis no longer

necessarry to layout the sail as a whole in the loft for

speci-fying the luff, leech and foot of the sail. Even all positions of

battens, reinforcements patches and reefs can be drawn upon the

individual panels before sewing the sail together, which means a

considerabLe saving of time and space in the saillofts.

The output of the computerprogram is a digital format: at regular intervals the coördinates of the points forming the sides of each panel are presented. Plotting these pointsby hand is a labouroüs

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affair, which has been done many times in the beginning stages of the project and yielded very good results.

But the output is much more suited for numerically controlled

cut-ting of the panels by machines such as known for instance in the

shipbuilding- and clothing iidiistry.

By coupling the computer, which calculates the pane:is,. direct to

a numerically controlled cutting machine, using a hot-knife or a laser beam,the pàneiscan be cut instantaneously.

(8)

-2. The Design process

First step in making a sail by using the method described in this paper is defining the shape of the sail in three dimensions and

to check whether the desrigned sail is feasable as a membrane under tension, i. e. that no hollows anywhere in the sail do occur.

This is one of the major problems in the new method since

sail-makers were not used to specify the section shape, amount of camber, position of maximum. camber and twist over the height of the sail.

So no experience did exist,, from which these data could be

collec-ted.

One way to obtain this information is by using the method asfirst

described by Haarstick in Ref. fiJ . He sets-up a kind of.

lines-plan of the combined sails in three dimensions of the yacht under consideration using all the information available of the yachts rig and deck layout. in the set-up of the linesplan he tries to take account of the mutual interaction between the mainsail and

the genoa. An example of such a drawing is presented in Figure 1.

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### maximum camber and the position of maximum camber must be specified.

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-The cross-section in the program are defined as nondimensional. of

f-sets. This means that the length of the cord is equal to unity and

the depth offsets are related. to this length of the cord and

re-present the cross-section of a foil with a maximum camber of 10% positioned at half the length along the cord. As an example the nondimensional circular are is presented in figure 2. For different percentages of camber and position of camber at a given

cross-sec-tion in the sail as may be specified by the designer, this standard

shape is transformed by multiplying all off sets with a constant factor calculated from the difference in camber, i.e. 1 .5 for 15%

camber instead of 10%, andby shifting all offsets over a. constant angle a as defined by the shift in position of maximum camber along the cord. This proceduce is visualised in figure 3. Finally by

multiplying all values with the actual cord length of the cross-section under consideration the actual cross-cross-section shape is ob-tained. The number of cross-sections thus dfined may be limited

to 5

Yc

or 6.

Y

0.1 0.2 0.3 0.6 05 06 07 0.8 0.9 1.0

Figur.e 2 Nbn dimensional cross-section shape(circular arc)

Dimensionless cross-section shape

choice: hyperbolic, circle etc.

max camber standard 10% camber 0.5 10 % camber Figure 3 1.0 00845 0.0961 0.10 0.061.9 0.0369

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(a) (b)

(d)

### Figure 4:a

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-8-All these data are used to calculate a three dimensional

presenta-tion of the sail. An example is presented in figure 4. The first drawing in this figure shows the input as given by the desigher, the other drawings are generated by the computer herefrom.

Emerging from the top of the sail twenty five radial cross-sections will be calculated using constant cordlines over the imputted

hori-zontal cross-section. By means of a spline interpolation poly-nominal expressions of the third order for each point of these

radial cross-sectionsthe depth can be determined. Using these ver-tical sections a large number of equidi:stant horizortal cross-sections £.sbeing calculated and plotted.

By means of the limited number of horizontal cross-sectional shapes as defined' by the designer the depthof any point in the sail can be calculated by finding the cord fraction of the section for the point in which the depth must be calculated. The depth is

calcu-lated by constructing a constant cord cross-section emerging from the top over the horizontal input sections using that particular

cord fraction. By means of the T.heilheimer spline interpolation

polynomal the depth atthe specific point is found. Using this tech-nique only a limited number of coefficients in the polynomial

expres-sion has to be calculated, which decreases the time necessarry for

the calculations, See figure 5.

Now the depth of the sail is known at any point a limited number of radial cross-sections emerging from the clew and the tack will also be calculated. Fig 4D and 4E. Ailthese cross-sections are used to check the designed sail on its designed shape and on the possible occurrance of hollow regions both visually by means of:the piots

or by calculating the second order' derivative o'f.each: cross-sec-tional shape.

If these regions are found' the shape of the sail must be changed. The perspective views are' added to give the designer an impression' of the shape of the sail he designed when looked upon from

diffe-rent standpoints Figure 4F and 4G. If the shape of the designed

sail is in correspondence with the shape wanted.

The designer 'passes on to the panel calculation procedure.

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10'-cord fraction of point p. In whichdept'h is to be known a:b Theilheimer f(x) - C1 + C2x + C3x2 + C4x3 +C5(,x - x3) +--CN_l(X where: + CN(X 3

### 3.

- x1) = (x - x) if x >

### ifx<=x1

Constant cordline used to .cicuIate depth at any point in the sai,i

### Figure 5: procedure to find depth in any point of the sail.

3

- xN_2)+

3 - XN_3)

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3. Panel definition

This routine in the computerprogram calculates the outline of the

panels of which the sail, is to be constructed. A large variety of

panel orientations can be used, i.e. horizontal, vertical, radial

from all corners and combinations'of all these.

The only limitation imposed on the designer when plannin the panel

layout is that the sail must be "buildable". This means that panels which are no developable surfaces by theIr nature may not be used,

i.e. building half a sphere from one panel is not possible but approximating this half sphere to a very large extend by using a

number of radial panels emerging from the center is quite well

feasible. In the procedure, which will be described in more detail

in paragraph 4, the computer calculates the shape of each panel which is uniquely defined by the shape in three dimensions of its

four (or three) sides, i.e. the seams.

The designer now specifies from where to where each seam of the

pa-ne.l extends into the sail designed.. In the vertical projection of the sail in the(x-z plane) the seams of each panel must be defined.

This is done by entering in succesive order the pointswhere the seams doterminate and specifying at the same time by means of a

code whether it is positioned on the leech (2), the luff (1), the foot (3) or somewhere in the middle of the sail (4). Also the. cha-racter of t:he seams spanning these points must be specified by a digital code dependent on whether they are part of the leech (2), the luff (1), the foot(3), the..sail surface (4) or part of a radial patern of panels emerging from a corner (5)

Seams of type 1, 2 and 3 are completly.de fined in three dimensions

already by the fact that they are part of the given edges of the

sail. The shape of seams of type number 4 and 5 must be calculated

by adding to their straight (4) of curved (5) projection in the x-z

plane the depth of the sail at a large number of points along the line of the seam using the method earlier described. Finally the

direction in which the panel can best be developed is added to

these data.

In figure 6 the different types of terminating points of the seams are visualised and in Figure 7 the different types of seams are presented.

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12-The panel is now compIetly defined by the shape of its boundaries

in three dimensions. By considering it to by a developable surface the shape of the panel can now be calculated.

Figure 6 types of seam terminating points

Figure. 7 types of seams

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13-4'. Panel. calculation

The. method used in our program to develop the panels of the sail

originates from the shipbuilding industry. A large variety of

methods to develop the. rather complex three dimensional shape of a ship into a plate are available. The method used in our program is the so called "cross-mould-method" and is used here because it

lends itself quite well for numerical compulations.

Only a short outline of, the procedure will be given in this paper.. For more detailed' Information eference is made to the literature

[2j

The method is based on covering the surfac.e of the pa'ne:l by a large

number of adjacent triangies andL developing the length's of the sides of all these triangles using, an approximation for the length of a curved line though three well defined points in space.. The

geo-metry of the triangles is completely defined by the length of their

respective sIdes. By using a large number of overlppirig triangles

and coupling all these together over the length. of the panel,

star-ting from a well defined straight line, the shape of the 'panel may

be laid off.

In our situation the surface to be developed' is a part of the sail, for instance such a's shown in figure 8.. This is just.one of the

many situations that might occur, but in principle these are all

simular.

14

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The panel is defined in space by the curvature along the four sides

AB, BD,. CD, AC. and the geometry of the surface in between these

boundaries.This part may e isolated as shown in figure 9.

y

FIgure 1.0

The depth (y) of the profile at each point of the section is calcu-lated using the routine mentioned earlier and by doing so all the

point's are explicitly de;fined by their 'x1 y and z coordinates re-,s.pectively. Note that only the depth at the specific points needs to be known.

Curved lines are drawn which do interconnect these points .as shown

in figure. 11 (for a small part..of the panel only) .

Figure 9

Both sections AB and CD. are now disc.reticed in a to.talof 25 points along the. cords at regular intervals and the corresponding points

of. both cords connected by straight lines. Half way in between both

sections a new auxiliary section is defIned to increase the

accu-racy. This is shown in figure 10.

15

-section 2

auxiliary section sectIon 1

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FIgure. 1.1

The developed length of all the line, segments between the points

A, E is calculated. To do this use is made of the developed length of the curve of a.parabolic function spanned by three. point's

in, space.

For instance for length of the.segment'AI the points A,. I and L are used, to define the parabolic function,' for 'segment El the

points E:, I. and J and, soon.

The developed length is calculated using the. known formula for the length of a parabolIc curve between three points, i.e..:

y .=p1 x +,p2x2

-x 'ab

### +f

dc '

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The discpncies between. the length of the actual curve through the three points and that of theparabolic function are neglectible in all practical cases if the points are not to far separated along

the cords.

Using this formula all the lengths of the generated triangles are

calculated respectively,.

The layout of the panel is now constructed by adding all these triangles together. Beginning with a stright line AC the

devel.-oped lengths of the sides of the first triangle ACI are set-out

as straight lines to yield point I. See figure 1.2.

Figure 12

The other triangles CXI and AGI. ar.e added yielding KG. Starting, from

here

### KGJ, KU

and GHJ. are laid of f.Consequently the shape. of the

part of the panel ACLH arises.

However a correction has to be made because the. developed length

of Al hs been set-out as:a straight line, but since point A, I

and L are not on a straight line the actual distance between

### A, C

and I must be. corrected for this discrepancy. This is done using the same parabolic function as described before.

The correction is applied to the lines Al and Ci and by doing so the position of point I is corrected to yield a new triangle with the exact developed lengths between points A, C and I, measured along the actual surface, now corresponding to the lengths along

the curved lines connecting these points.

This. yields a new line KIG which On its turn now is the starting line for the. next triangulation.

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-This procedure is repeated for all triangles.

The final result is the shape of the developed panel.

The output of the procedure is the shapes of the. panel in a large number of offsets representing the boundaries of the panel.

These may either be plotted by hand or directly iinked to an

(22)

5. Examples

From experience gained during full scale experiments with a number of different sails with various dimensions, it appeared that the

results of the panel calculation method are very accurate.

The panels of the sail fit together without any problem. Adjecent sides of two panels, forming one seam together, are exactly of the same length. The layout of the sail is in correspondence with the design and so are the overall dimensions. Finally the shape

desig-ned into the sail corresponds with the shape of the actual product:.

This may be seen when companning the shape in photographs with the plots of the designed sail. Seefigure 14.This 'is the main-sail of a fractional rig9ed three quarter tonner.

The other sail in figure 15,is the.designof.a surf.sail.

From all the tests with the testsails 'it. appeared that the actual

shape of the sails corresponds very much to the designed shapeal-though some corrections in the design are necessarry to compensate

for distortion .of the sail under load. Further distortion of the sail under actual sailing conditions can. be corrected in the same way as with usual sails, i.e. hailyard tension, sheet tension,

lead position etc., the same t'instruments" thatmaybe used to

change. the shape of the sail if felt necessarry.

The construc.tion of the sails .tended to take less. time since laying

out the complete sail on the floor forcuttingthe leeches etc. was no longe.r necessarry. On thevthèr hand it.took.a little more

time to s.ew the sometimes rather curved. seams 'together.

As an advantage of using a computer,in the...designprocess of a sail it should be mentioned that',it 'is very easyto reproduce sails if

wanted, because all the data may bestored. either on permanent

me-mory of the computer or on paper as plot's and: . tables. and remains

available at any time without much difficulty. If comments concer-ning the actual product afloat are added to this data a valuable databank arises within a short time from which much knowledge may

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Surf sail

Input data

Figure 14a

2O

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The shape of the radial cross sections

Panel definition

Figure i4b

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Input data

.I I

### i4

Figure 15a Vertical and horizontal - 22 - cross sections.

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T.he shape. of the. radial dross sections

Figuxe 15b 23

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6. Future Developments

Because of the fact that a method to design Sails and to calcu-late the shape of the panels is now available a number of other

possibilities arise.

First of all, it has been mentioned before, a numerically controlled

automatic cutting machine for the panels is feasible. This is not new, such machines do exist already, but in most cases they use

moulds as an input. In combination with the panel calculation method

however it is possible tocut. any panel of any sail, direct from the

drawing board on which the design originates. Such a cutting machine equiped with a laser beam cutting device is now under cons:trution

at Gaastra Sails BV at Sneek.

As has been outlined before the fact, that any shape designed can now

be reproduced in the sails, makes it possibLe to experiment with different sail shapes and combinations while knowing exactly what shape is "on". By doing full scale experiments with different sails

or combinations of sails a much more reliable and accurate search

for the optimum- shapes can be performed than in the case with the

In the search for stronger and lighter sails it is a great benefit to be able to change the panel layout and orientation whie knowing that the shape of the sail remains unchanged. This too enables a quicker and more reliable search for the optimum.

When a large amount of experience has been gained in.the design and the construction of the sails, it maybecome'feasib1e to

nondimen-sionalize a proven design of an explicit type .of sail, for instance a genoa light, a genoa heavy, a mast top main etc.

The sail must benondimensionalised using a number of

main-dime.-sions of the sail.

When such a nondimensional sail is stored in the computermemory, a new sail with different dimensions may easily be. generated using

the proper dimensions of the sail wanted. The design process may

be shortened considerably using this techique. The new sail wil.i

fulfill all the requirements of the sail wanted since it is proven

by previous experience.

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-7. Acknowledgement

The contribuions and guidance of Prof. i,r. J. Gerritsma is

grate-fully acknowledged.

The cooperation with Gaastra Sails in this project was highly

appreciated by the authors.

(29)

References

[i} PrInciples of Sail Design

Stephen Haarstick

Chesapeake Sailing Yachte Symposium

SNAME januari 1977

2J Beschrijving compute]programrna voor het berekeren van de baanuitslagen van zeilen.

A. Ve:rsluis

Report No. 505-M juli 19.80

.Laboratoriurn Scheepshydromechanica

TH-Delft

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