Table 3.

Numerical calculated values of$\overline{C_{hkl}}$, $q_1$ and $q_2$ for the most common slip systems in titanium [20].

Slip System	Slip Plane	Burger Vector	${\overline{\mathit{C}}}_{\mathit{h}\mathit{k}.0}$	${\mathit{q}}_1$	${\mathit{q}}_2$
Basal <a>	$\left(0002\right)$	$\left[11\overline{2}0\right]$	0.20227	−0.101142	−0.102623
Prismatic <a>	$\left(1\overline{1}00\right)$	$\left[11\overline{2}0\right]$	0.35387	−1.19272	0.355623
Prismatic <c>	$\left(1\overline{1}00\right)$	$\left[0001\right]$	0.04853	3.61619	1.226411
Prismatic <c + a>	$\left(1\overline{1}00\right)$	$\left[11\overline{2}3\right]$	0.10247	2.01717	−0.616631
Pyramidal1<a>	$\left(10\overline{1}1\right)$	$\left[11\overline{2}0\right]$	0.3118	−0.89401	0.183311
Pyramidal2 <c + a>	$\left(11\overline{2}2\right)$	$\left[11\overline{2}3\right]$	0.09227	1.29905	0.397247
Pyramidal3 <c + a>	$\left(11\overline{2}1\right)$	$\left[11\overline{2}3\right]$	0.09813	1.89412	−0.365739
Pyramidal4 <c + a>	$\left(10\overline{1}0\right)$	$\left[11\overline{2}3\right]$	0.09323	1.52702	0.146150
Screw <a>	Multiple	$\left[11\overline{2}0\right]$	0.1444	0.59492	−0.710368
Screw <c + a>	Multiple	$\left[11\overline{2}3\right]$	0.41873	1.25714	−0.94015
Screw <c>	Multiple	$\left[0001\right]$	3.61 × 10−6	165366	−98611