Answer:
(a) Shear plane angle will be 21.9°
(b) Shear train will be 2.7913 radian
Step-by-step explanation:
We have given rake angle
![\alpha =5^(\circ)](https://img.qammunity.org/2020/formulas/engineering/college/3o2hqusybng7ut26efegz4mtr97418pew8.png)
Thickness before cut
![t_1=0.01inch](https://img.qammunity.org/2020/formulas/engineering/college/8vuacuyt8tx7i7fv7mtwr4f7e1bqnpwj55.png)
Thickness after cutting
![t_2=0.027inch](https://img.qammunity.org/2020/formulas/engineering/college/q3c7ll19lcjqxzi5h7k0g0wyid6jj7drp7.png)
Now ratio of thickness before and after cutting
![r=(t_1)/(t_2)=(0.01)/(0.027)=0.3703](https://img.qammunity.org/2020/formulas/engineering/college/xzaqngzj3txmnge79acctrlatm3ubsonpi.png)
(a) Shear plane angle is given by
, here
is rake angle.
So
![tan\Phi =(0.3703* cos5^(\circ))/(1-sin5^(\circ))=0.4040](https://img.qammunity.org/2020/formulas/engineering/college/h54dnho2tfyg4nsnn1sk6wy1dols1x9950.png)
![\Phi =tan^(-1)0.4040](https://img.qammunity.org/2020/formulas/engineering/college/xgdqcywn1byz7cactphcxz2mxrsx5yhc8s.png)
![\Phi =21.9^(\circ)](https://img.qammunity.org/2020/formulas/engineering/college/jzhwr80l35f8plnxfcq5yy711fi89xl20x.png)
(b) Shear strain is given by
![\gamma =tan(\Phi -\alpha )+cot\Phi](https://img.qammunity.org/2020/formulas/engineering/college/ii8ohtwsw5d9nk0gxihylg2mk44wokefmv.png)
So
![\gamma =tan(21.9 -5 )+cot21.9=2.7913radian](https://img.qammunity.org/2020/formulas/engineering/college/okys9a23s75l1dsrltz9mgmuvo2lngmm88.png)