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The Delft Sand, Clay & Rock Cutting Model, 2019a

The Delft Sand, Clay & Rock Cutting Model, 2019a

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sin <br />

<strong>Rock</strong> <strong>Cutting</strong>: Atmospheric Conditions.<br />

sin sin<br />

2 0<br />

<br />

(8-89)<br />

<br />

(8-90)<br />

2 2<br />

Using this, gives for the force F:<br />

F <br />

<br />

<br />

<br />

<br />

<br />

1 2ch i wcos <br />

<br />

n 1 1 cos <br />

(8-91)<br />

This gives for the horizontal force Fh and the vertical force Fv:<br />

1 2ch wcos( )sin( )<br />

1<br />

F c h w<br />

i<br />

h HF i<br />

n 1 1 cos( ) n<br />

1<br />

(8-92)<br />

(8-93)<br />

This solution is the same as the Merchant solution (equations (8-109) and (8-110)) that will be derived in the next<br />

chapter, if the value of the stress distribution factor n=0. In fact the stress distribution factor n is just a factor to<br />

reduce the forces. From tests it appeared that in a type of rock the value of n depends on the rake angle. It should<br />

be mentioned that for this particular case n is about 1 for a large cutting angle. In that case tensile failure may give<br />

way to a process of shear failure, which is observed by other researches as well. For cutting angles smaller than<br />

80 degrees n is more or less constant with a value of n=0.5. Figure 8-31 and Figure 8-32 show the coefficients λHF<br />

and λVF for the horizontal and vertical forces Fh and Fv according to equations (8-109) and (8-110) as a function<br />

of the blade angle α and the internal friction angle φ, where the external friction angle δ is assumed to be 2/3·φ. A<br />

positive coefficient λVF for the vertical force means that the vertical force Fv is downwards directed. Based on<br />

equation (8-97) and (8-109) the specific energy Esp can be determined according to:<br />

E<br />

sp<br />

Pc Fh vc Fh<br />

1<br />

HF<br />

c<br />

Q h w v h w n<br />

1<br />

i c i<br />

<br />

<br />

(8-94)<br />

1.0<br />

Stress Distribution Nishimatsu<br />

0.9<br />

0.8<br />

0.7<br />

p/p 0<br />

0.6<br />

0.5<br />

0.4<br />

0.3<br />

n=0.00<br />

n=0.25<br />

n=0.50<br />

n=1.00<br />

n=2.00<br />

n=4.00<br />

n=8.00<br />

0.2<br />

0.1<br />

0.0<br />

0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0<br />

Distance along the shear plane<br />

© S.A.M.<br />

Figure 8-25: <strong>The</strong> stress distribution along the shear plane.<br />

Copyright © Dr.ir. S.A. Miedema TOC Page 271 of 454

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