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 PART - II

APPENDIX II - 1

Derivation of the algebraic expressions in the general equation
for Brown’s data

In our first attempt to derive algebraic expressions for F1, U, LM,lm in terms of readily measurable cotton fibre-characteristics we made use of data reported by Brown [7]. Brown and coworkers spun each of six cottons to three counts, NE 18, NE 36, and NE 72; and each count to a number of twist multipliers ranging from 2.75 to 5.75. The fibre test data on the six cottons are reproduced in Table II– A – 1 - i and the yarn CS in Table II – A – 1 - ii

For any cotton, at any one count, the plot of CS against M, the twist multiplier, yields the typical ‘inverted parabola’ -- the smooth curves in Figure II – a – 1 - i for example, with the curve of a finer count being below that of a coarser count. We have seen that the general equation for these curves is

We can rewrite this equation as

As M increases, U and (lm + LM tend to their respective asymptotic minimum values, namely, zero and lm. Therefore, for any one count, as M increases,

tends to its maximum value for that count, namely,

For convenience we write

Then,

If, therefore, for yarn of any one count, we plot the quantity (CS x D) against M, we will get a curve that reaches this asymptotic maximum - - Table II – A – 1 - iii, and Figure II – A – 1 - ii. This is what would happen if there were no obliquity effect. With increasing twist, the fraction of fibres that slip, and the length of fibre-element that breaks when yarn fails in tenacity testing, will both reach their respective minimum; therefore the CS will reach its maximum, and with further increase in twist will continue to remain the same.

For any cotton, from plots of {(CS x D)} against M, Figure II – A – 1 - ii, we can read off the numerical value of X for each of the three counts spun from that cotton. We can do this for each of the six cottons. These values are also given in Table II – A – 1 - iii.

At any intermediate value of M,

Substituting for F2 and F3,

The important point to note is that, for any yarn, we can calculate the numerical value of the RHS of this equation from its CS and M. Therefore, we can prepare a table giving the experimental values of  for each of the 133 yarns in Brown’s spinnings - -  six cottons, each spun to three counts, and each count to a number of twists. These values are in Table II – A - 1 - iv. We use these reference data to formulate algebraic expressions for U,Lm,lm  We do this by trial and error until the numerical value of the LHS calculated from the algebraic expressions is as close to the corresponding experimental value in the RHS, for each of 133 yarns.

In this context, we recall the earlier enunciated premises regarding U,lm,and LM.  The fall of U with increasing M is governed by fibre-length, fibre-fineness and yarn count. Based on the observation that all fibres appear broken when the two ends of a broken high-twisted yarn is examined, we assume that the asymptotic minimum value of U=0  However, the asymptotic minimum value of the gauge-length of fibre-break in yarn-break as M tends to infinity, is not zero, but a finite value lm. This value is dependent upon fibre-fineness. Furthermore, LM, the increment over lm at any other discrete value of M is dependent upon fibre-fineness and yarn-count, but not on fibre-length. Therefore, fibre-length does not influence the fall of (LM+ lm) to lm with increasing twist.

The final set of equations that we constructed for U,lm,and LM is follows:-

Let us denote the fibre effective length in mm by L0, the fibre fineness in millitex by H, the Stelometer zero-gauge tenacity in g/t by Z, and the gauge-length effect on fibre tenacity by G.

Figure II – A – 1 - iii is a plot of the observed value of  against M, for Akala cotton; over the points, is the smooth curve generated by the algebraic expression for estimating , F2 x f3 namely   . The smooth curve for each one of the three counts passes quite close to the points representing the observed values. A point of interest is that at twists of 2.75 and 3.25 the estimated value of F2 x f3 decreases from NE 18 to NE36, and again from Ne 36 to NE 72. This trend is discernible in the observed values when one scans the data over all the six cottons - - Table II A – 1 – iv. The estimated values of F2 x f3, namely, are in Table II – A – 1 – v. In each of the available 133 cases, the estimated value  is in good agreement with the observed value  namely, . The scatter diagram of estimated against observed, Figure II – A – 1 – iv, has a straight line, Y = 0.997 x X. Plotted serially, the observed and estimated values almost merge into each other. The functions

and the algebraic expressions for U,lm,and LM are, therefore, valid to quantify the increase of CS with increasing M. We already have,  to quantify the fall in CS with M as a result of fibre obliquity.

We have, thus, algebraic expressions for F2,F3 and F4 in terms of fibre-characteristics and yarn- count and twist to quantify the three-fold contribution of twist to yarn tenacity.

It now remains to derive the expression for F1, the irregularity fraction. For this we recall that

Therefore, for yarns of the three counts spun from any one cotton, a plot of  The numerical values of the intercept and slope of the line can be related to cotton characteristics, to give us F1. The actual plots did yield straight lines for all the six cottons. The algebraic expression for the irregularity fraction turned out to be 

a = -0.209, b = 0, and L is effective length in mm.

Therefore the final equation is

Also

 

Cotton

Acala

Delta-
Pine

Hopi

Karnak

Wilds

Inter-
Species

E.L. mm

33.73

33.34

33.34

38.10

34.93

30.96

Fineness
millitex

186

204

199

139

165

156

“0-gauge’ tenacity g/t

40.5

35.3

48.9

44.7

39.1

53.5

2.5-mm tenacity g/t

19.8

18.9

23.6

26.2

21.8

23.7

Table II – A –1 - i  Brown’s Data :
Fibre-Characteristics of Cottons  Used In The Spinnings

 

Notes :-
 Source ; Tex. Res. J., April, 1957, Page 332
 E.L., comb sorter effective length, mm. = UHML, inches x 1.154 x 25.4
             Fineness, millitex = Suter-Webb micro-g/inch x 39.4 x 1.10
             0-gauge tenacity g/t, Stelo level = Pressley Index x 5.36 x /1.152
             2.5-mm tenacity g/t, Stelo level = Pressley 2.5-mm g/t / 1.26

 

COTTON

 

C

 

M

2.75

3.25

3.5

3.75

4.00

4.25

4.75

5.75

Akala

18

2225

2625

2800

2850

2875

2900

2800

2600

 

36

NA

2275

2325

2400

2450

2475

2400

2200

 

72

NA

1650

1850

1875

1975

1975

1875

1625

Delta

18

1925

2350

2500

2525

2525

2550

2550

2350

 

36

NA

1950

2075

2125

2150

2200

2125

1950

 

72

NA

NA

1650

1700

1725

1725

1650

1400

Hopi

18

2350

3100

3275

3250

3275

3325

3200

2825

 

36

NA

2600

2750

2825

2775

2850

2700

2450

 

72

NA

1700

2000

2125

2200

2200

2075

1775

Interspec

18

3025

3600

3775

3725

3700

3700

3600

3175

 

36

2300

3200

3275

3325

3375

3400

3200

2800

 

72

1550

2350

2600

2550

2650

2625

2475

2150

Karnak

18

3225

3550

3600

3575

3550

3450

3450

3150

 

36

2775

3125

3200

3150

3150

NA

2925

2600

 

72

2300

2625

2650

2650

2700

NA

2525

2200

Wilds

18

2500

2850

2850

2925

2925

2900

2850

2525

 

36

2000

2450

2500

2525

2575

NA

2425

2250

 

72

1450

1900

1950

2000

2050

NA

1950

1650

TABLE –  II – A - 1 – ii Brown’s Data: Experimentally Observed CS

OBS(CS*D)

 

C

 

(CS x D) AT M

(CSXD) max

COTTON

2.75

3.25

3.50

3.75

4.00

4.25

4.75

5.75

Akala

18

2461

3013

3280

3411

3519

3633

3684

3803

3750

 

36

NA

2611

2724

2873

2999

3101

3158

3218

3200

 

72

NA

1894

2167

2244

2417

2474

2467

2377

2500

Delta

18

2129

2698

2929

3022

3091

3195

3355

3438

3350

 

36

NA

2238

2431

2543

2632

2756

2796

2853

2800

 

72

NA

NA

1933

2035

2111

2161

2171

2048

2200

Hopi

18

2599

3558

3837

3890

4009

4166

4211

4133

4200

 

36

NA

2984

3222

3381

3397

3571

3553

3584

3600

 

72

NA

1951

2343

2543

2693

2756

2730

2597

2775

Interspec

18

3345

4132

4422

4458

4529

4636

4737

4645

4750

 

36

2544

3673

3837

3980

4131

4260

4211

4096

4250

 

72

1714

2698

3046

3052

3244

3289

3257

3145

3300

Karnak

18

3566

4075

4217

4279

4345

4322

4540

4608

4500

 

36

3069

3587

3749

3770

3856

NA

3849

3803

3925

 

72

2544

3013

3104

3172

3305

NA

3323

3218

3350

Wilds

18

2765

3271

3339

3501

3580

3633

3750

3694

3750

 

36

2212

2812

2929

3022

3152

NA

3191

3291

3250

 

72

1604

2181

2284

2394

2509

NA

2566

2414

2550

TABLE II – A - 1 – iii Observed Values of (CS x D)

 

.Obs F2*f3

 

m

 

 

 

 

 

 

 

COTTON

c

2.75

3.25

3.5

3.75

4

4.25

4.75

5.75

Akala

18

0.656

0.804

0.875

0.910

0.938

0.969

0.983

1.014

 

36

0.000

0.816

0.851

0.898

0.937

0.969

0.987

1.006

 

72

0.000

0.758

0.867

0.898

0.967

0.990

0.987

0.951

Delta

18

0.635

0.805

0.874

0.902

0.923

0.954

1.002

1.026

 

36

0.000

0.799

0.868

0.908

0.940

0.984

0.999

1.019

 

72

0.000

0.000

0.879

0.925

0.960

0.982

0.987

0.931

Hopi

18

0.619

0.847

0.913

0.926

0.954

0.992

1.003

0.984

 

36

0.000

0.829

0.895

0.939

0.944

0.992

0.987

0.996

 

72

0.000

0.703

0.844

0.917

0.970

0.993

0.984

0.936

Interspec

18

0.704

0.870

0.931

0.939

0.953

0.976

0.997

0.978

 

36

0.598

0.864

0.903

0.936

0.972

1.002

0.991

0.964

 

72

0.519

0.817

0.923

0.925

0.983

0.997

0.987

0.953

Karnak

18

0.793

0.906

0.937

0.951

0.966

0.961

1.009

1.024

 

36

0.782

0.914

0.955

0.961

0.982

0.000

0.981

0.969

 

72

0.759

0.899

0.927

0.947

0.987

0.000

0.992

0.961

Wilds

18

0.737

0.872

0.890

0.934

0.955

0.969

1.000

0.985

 

36

0.681

0.865

0.901

0.930

0.970

0.000

0.982

1.013

 

72

0.629

0.855

0.896

0.939

0.984

0.000

1.006

0.947

TABLE II – A – 1 – iv Experimentally observed values of F2 x f3

 

EST  F2*f3

 

m

 

 

 

 

 

 

 

name

c

2.750

3.250

3.500

3.750

4.000

4.250

4.750

5.750

Akala

18

0.660

0.850

0.899

0.930

0.950

0.964

0.980

0.993

 

36

0.600

0.821

0.881

0.917

0.941

0.957

0.977

0.992

 

72

0.528

0.786

0.860

0.902

0.930

0.950

0.972

0.990

Delta

18

0.654

0.847

0.898

0.929

0.950

0.964

0.980

0.993

 

36

0.593

0.818

0.880

0.916

0.940

0.957

0.976

0.992

 

72

0.517

0.782

0.858

0.901

0.929

0.949

0.972

0.990

Hopi

18

0.622

0.830

0.886

0.920

0.943

0.959

0.978

0.992

 

36

0.559

0.799

0.866

0.906

0.933

0.952

0.973

0.991

 

72

0.483

0.760

0.842

0.889

0.921

0.943

0.968

0.989

Interspec

18

0.688

0.866

0.911

0.939

0.956

0.969

0.983

0.994

 

36

0.627

0.839

0.895

0.927

0.948

0.963

0.980

0.993

 

72

0.548

0.804

0.876

0.914

0.939

0.956

0.976

0.991

Karnak

18

0.821

0.925

0.950

0.966

0.976

0.983

0.990

0.997

 

36

0.786

0.910

0.941

0.959

0.971

0.979

0.989

0.996

 

72

0.743

0.893

0.930

0.952

0.966

0.975

0.987

0.995

Wilds

18

0.753

0.895

0.930

0.952

0.966

0.975

0.987

0.995

 

36

0.706

0.874

0.917

0.943

0.960

0.971

0.984

0.994

 

72

0.646

0.849

0.902

0.932

0.952

0.965

0.981

0.993

TABLE II – A – 1 - v Estimated values of F2 x f3

Figure II – A – 1 - i Inverted parabola shape curves of CS – M plot

 

Figure II – A – 1 - ii Plot of (CS X D) against M

 

Figure II – A – 1 - iii Plot of F2 x f3 against M
with smooth curves from expression for F2 x f3 drawn over the points

 

Figure II – A – 1 – iv Showing good agreement between observed and estimated
values of F2 x f3

PART - II
Conceptual Framework and Methodology Used to Derive the Algebraic Expressions
 
Chapter 1
Chapter 2
Chapter 3
Chapter 4
Chapter 5
Chapter 6
APPENDIX II - 1
APPENDIX II - 2
APPENDIX II - 3
APPENDIX II - 4
APPENDIX II - 5
 
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