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Copy to Native Excel:
Click in the text area below and copy. Then paste into cell A1 of a worksheet. All the formulas are brought in intact but Excel default behaviour controls formatting. A better transfer can be achieved using our XLC add-in for Excel (see below).

<table><tbody><tr><td></td>	<td>Length of sides</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>b =</td>	<td>30</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td>d =</td>	<td>50</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td>d1 =</td>	<td>20</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td>b1 =</td>	<td>5</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Area and distances from centroid to extremities </td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Area of Rectangle</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>A =</td>	<td>=D2*D3-D5*D4</td>	<td>mm²</td>	<td>in²</td></tr>
				<tr><td></td>	<td>Distance to Extreme Fiber</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>y1 =</td>	<td>=(D3)/(2)</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>y2 =</td>	<td>=(D2)/(2)</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Moments and products of inertia and radii of gyration about central axes </td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Moment of inertia</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>I1 =</td>	<td>=(D2*D3^3-D5*D4^3)/(12)</td>	<td>mm⁴</td>	<td>in⁴</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>I2 =</td>	<td>=(D3*D2^3-D4*D5^3)/(12)</td>	<td>mm⁴</td>	<td>in⁴</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Radius of gyration</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>r1 =</td>	<td>=SQRT((D17)/(D9))</td>	<td>mm</td>	<td>mm</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>r2 =</td>	<td>=SQRT((D19)/(D9))</td>	<td>mm</td>	<td>mm</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Plastic section moduli shape factors, and locations of plastic neutral axes</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Plastic section modulus </td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Z1 =</td>	<td>=(D2*D3^2-D5*D4^2)/(4)</td>	<td>mm³</td>	<td>in³</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Z2 =</td>	<td>=(D3*D2^2-D4*D5^2)/(4)</td>	<td>mm³</td>	<td>in³</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Shape Factor</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>SF1 =</td>	<td>=(D28*D3)/(2*D17)</td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>SF2 =</td>	<td>=(D30*D2)/(2*D19)</td>	<td></td>	<td></td></tr></tbody></table>

Copy to XLC Enhanced Excel:
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<table><tbody><tr><td></td>	<td>Length of sides</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>b =</td>	<td>30</td>	<td>mm</td>	<td>in</td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>d =</td>	<td>50</td>	<td>mm</td>	<td>in</td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>d1 =</td>	<td>20</td>	<td>mm</td>	<td>in</td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>b1 =</td>	<td>5</td>	<td>mm</td>	<td>in</td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Area and distances from centroid to extremities </td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Area of Rectangle</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>A =</td>	<td>=D2*D3-D5*D4</td>	<td>mm²</td>	<td>in²</td>	<td>=EQS(D9,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$33_2")</td></tr>
				<tr><td></td>	<td>Distance to Extreme Fiber</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>y1 =</td>	<td>=OVD(D3)/UND(2)</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D11,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$36_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>y2 =</td>	<td>=OVD(D2)/UND(2)</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D13,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$37_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Moments and products of inertia and radii of gyration about central axes </td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Moment of inertia</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>I1 =</td>	<td>=OVD(D2*D3^3-D5*D4^3)/UND(12)</td>	<td>mm⁴</td>	<td>in⁴</td>	<td>=EQS(D17,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$45_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>I2 =</td>	<td>=OVD(D3*D2^3-D4*D5^3)/UND(12)</td>	<td>mm⁴</td>	<td>in⁴</td>	<td>=EQS(D19,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$47_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Radius of gyration</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>r1 =</td>	<td>=SQRT(OVD(D17)/UND(D9))</td>	<td>mm</td>	<td>mm</td>	<td>=EQS(D22,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$51_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>r2 =</td>	<td>=SQRT(OVD(D19)/UND(D9))</td>	<td>mm</td>	<td>mm</td>	<td>=EQS(D24,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$52_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Plastic section moduli shape factors, and locations of plastic neutral axes</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Plastic section modulus </td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Z1 =</td>	<td>=OVD(D2*D3^2-D5*D4^2)/UND(4)</td>	<td>mm³</td>	<td>in³</td>	<td>=EQS(D28,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$56_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Z2 =</td>	<td>=OVD(D3*D2^2-D4*D5^2)/UND(4)</td>	<td>mm³</td>	<td>in³</td>	<td>=EQS(D30,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$58_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Shape Factor</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>SF1 =</td>	<td>=OVD(D28*D3)/UND(2*D17)</td>	<td></td>	<td></td>	<td>=EQS(D33,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$61_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>SF2 =</td>	<td>=OVD(D30*D2)/UND(2*D19)</td>	<td></td>	<td></td>	<td>=EQS(D35,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$63_2")</td></tr></tbody></table>

Units: SI(mm) & US(in) - delete as appropriate.

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<table><tbody><tr><td></td>	<td></td>	<td>Length of sides</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>b =</td>	<td>40</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>d =</td>	<td>50</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>t =</td>	<td>10</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>tw =</td>	<td>15</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Area and distances from centroid to extremities </td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Area</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>A =</td>	<td>=2*E2*E4+E5*E3</td>	<td>mm²</td>	<td>in²</td></tr>
				<tr><td></td>	<td></td>	<td>Distance to Extreme Fiber</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>y1 =</td>	<td>=(E3)/(2)+E4</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>y2 =</td>	<td>=(E2)/(2)</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Moments and products of inertia and radii of gyration about central axes </td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Moment of inertia</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>I1 =</td>	<td>=(E2*(E3+2*E4)^3)/(12)-((E2-E5)*E3^3)/(12)</td>	<td>mm⁴</td>	<td>in⁴</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>I2 =</td>	<td>=(E2^3*E4)/(6)+(E5^3*E3)/(12)</td>	<td>mm⁴</td>	<td>in⁴</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Radius of gyration</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>r1 =</td>	<td>=SQRT((E17)/(E9))</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>r2 =</td>	<td>=SQRT((E19)/(E9))</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Plastic section moduli shape factors, and locations of plastic neutral axes</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Plastic section modulus </td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>Z1 =</td>	<td>=(E5*E3^2)/(4)+E2*E4*(E3+E4)</td>	<td>mm³</td>	<td>in³</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>Z2 =</td>	<td>=(E2^2*E4)/(2)+(E5^2*E3)/(4)</td>	<td>mm³</td>	<td>in³</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Shape Factor</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>SF1 =</td>	<td>=(E28*E11)/(E17)</td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>SF2 =</td>	<td>=(E30*E13)/(E19)</td>	<td></td>	<td></td></tr></tbody></table>

<table><tbody><tr><td></td>	<td>Length of sides</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>b =</td>	<td>40</td>	<td>mm</td>	<td>in</td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>d =</td>	<td>50</td>	<td>mm</td>	<td>in</td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>t =</td>	<td>10</td>	<td>mm</td>	<td>in</td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>tw =</td>	<td>15</td>	<td>mm</td>	<td>in</td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Area and distances from centroid to extremities</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Area</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>A =</td>	<td>=2*D2*D4+D5*D3</td>	<td>mm²</td>	<td>in²</td>	<td>=EQS(D9,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$J$31_2")</td></tr>
				<tr><td></td>	<td>Distance to Extreme Fiber</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>y1 =</td>	<td>=OVD(D3)/UND(2)+D4</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D11,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$J$33_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>y2 =</td>	<td>=OVD(D2)/UND(2)</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D13,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$J$35_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Moments and products of inertia and radii of gyration about central axes</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Moment of inertia</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>I1 =</td>	<td>=OVD(D2*(D3+2*D4)^3)/UND(12)-OVD((D2-D5)*D3^3)/UND(12)</td>	<td>mm⁴</td>	<td>in⁴</td>	<td>=EQS(D17,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$J$39_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>I2 =</td>	<td>=OVD(D2^3*D4)/UND(6)+OVD(D5^3*D3)/UND(12)</td>	<td>mm⁴</td>	<td>in⁴</td>	<td>=EQS(D19,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$J$41_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Radius of gyration</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>r1 =</td>	<td>=SQRT(OVD(D17)/UND(D9))</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D22,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$J$44_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>r2 =</td>	<td>=SQRT(OVD(D19)/UND(D9))</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D24,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$J$46_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Plastic section moduli shape factors, and locations of plastic neutral axes</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Plastic section modulus</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Z1 =</td>	<td>=OVD(D5*D3^2)/UND(4)+D2*D4*(D3+D4)</td>	<td>mm³</td>	<td>in³</td>	<td>=EQS(D28,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$J$50_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Z2 =</td>	<td>=OVD(D2^2*D4)/UND(2)+OVD(D5^2*D3)/UND(4)</td>	<td>mm³</td>	<td>in³</td>	<td>=EQS(D30,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$J$52_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Shape Factor</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>SF1 =</td>	<td>=OVD(D28*D11)/UND(D17)</td>	<td></td>	<td></td>	<td>=EQS(D33,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$J$55_2")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>SF2 =</td>	<td>=OVD(D30*D13)/UND(D19)</td>	<td></td>	<td></td>	<td>=EQS(D35,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$J$57_2")</td></tr></tbody></table>

<table><tbody><tr><td></td>	<td></td>	<td>Length of sides</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>b =</td>	<td>80</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>d =</td>	<td>30</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>t =</td>	<td>10</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>tw =</td>	<td>15</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Area and distances from centroid to extremities </td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Area</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>A =</td>	<td>=E4*E2+2*E5*E3</td>	<td>mm²</td>	<td>in²</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Distance to Extreme Fiber</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>y1 =</td>	<td>=(E2*E4^2+2*E5*E3*(2*E4+E3))/(2*(E4*E2+2*E5*E3))</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>y2 =</td>	<td>=(E2)/(2)</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Moments and products of inertia and radii of gyration about central axes </td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Moment of inertia</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>I1 =</td>	<td>=(E2)/(3)*(E3+E4)^3-(E3^3)/(3)*(E2-2*E5)-E9*(E3+E4-E12)^2</td>	<td>mm⁴</td>	<td>in⁴</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>I2 =</td>	<td>=((E3+E4)*E2^3)/(12)-(E3*(E2-2*E5)^3)/(12)</td>	<td>mm⁴</td>	<td>in⁴</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Radius of gyration</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>r1 =</td>	<td>=SQRT((E17)/(E9))</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>r2 =</td>	<td>=SQRT((E19)/(E9))</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Plastic section moduli shape factors, and locations of plastic neutral axes</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Plastic section modulus </td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>Z1a =</td>	<td>=(E3^2*E5)/(2)-(E2^2*E4^2)/(8*E5)+(E2*E4*(E3+E4))/(2)</td>	<td>mm³</td>	<td>in³</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>Z1b =</td>	<td>=(E4^2*E2)/(4)+E5*E3*(E4+E3-(E5*E3)/(E2))</td>	<td>mm³</td>	<td>in³</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>Z1 =</td>	<td>=IF(2*E5*E3<=E2*E4,E28,E30)</td>	<td>mm³</td>	<td>in³</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>s1 =</td>	<td>=(E2*E4/2*E5+E3)/2</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>s2 =</td>	<td>=E5*E3/E2+E4/2</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>s =</td>	<td>=IF(2*E5*E3<=E2*E4,E34,E36)</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>Z2 =</td>	<td>=(E2^2*E4)/(4)+E5*E3*(E2-E5)</td>	<td>mm³</td>	<td>in³</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Shape Factor</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>SF1 =</td>	<td>=(E32*(E3+E4-E12))/(E17)</td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td>SF2 =</td>	<td>=(E40*E2)/(2*E19)</td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr></tbody></table>

<table><tbody><tr><td></td>	<td>Length of sides</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>b =</td>	<td>80</td>	<td>mm</td>	<td>in</td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>d =</td>	<td>30</td>	<td>mm</td>	<td>in</td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>t =</td>	<td>10</td>	<td>mm</td>	<td>in</td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>tw =</td>	<td>15</td>	<td>mm</td>	<td>in</td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Area and distances from centroid to extremities </td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Area</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>A =</td>	<td>=D4*D2+2*D5*D3</td>	<td>mm²</td>	<td>in²</td>	<td>=EQS(D9,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$34_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Distance to Extreme Fiber</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>y1 =</td>	<td>=OVD(D2*D4^2+2*D5*D3*(2*D4+D3))/UND(2*(D4*D2+2*D5*D3))</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D12,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$37_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>y2 =</td>	<td>=OVD(D2)/UND(2)</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D14,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$38_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Moments and products of inertia and radii of gyration about central axes </td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Moment of inertia</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>I1 =</td>	<td>=OVD(D2)/UND(3)*(D3+D4)^3-OVD(D3^3)/UND(3)*(D2-2*D5)-D9*(D3+D4-D12)^2</td>	<td>mm⁴</td>	<td>in⁴</td>	<td>=EQS(D18,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$42_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>I2 =</td>	<td>=OVD((D3+D4)*D2^3)/UND(12)-OVD(D3*(D2-2*D5)^3)/UND(12)</td>	<td>mm⁴</td>	<td>in⁴</td>	<td>=EQS(D20,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$43_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Radius of gyration</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>r1 =</td>	<td>=SQRT(OVD(D18)/UND(D9))</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D23,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$46_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>r2 =</td>	<td>=SQRT(OVD(D20)/UND(D9))</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D25,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$48_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Plastic section moduli shape factors, and locations of plastic neutral axes</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Plastic section modulus </td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Z1a =</td>	<td>=OVD(D3^2*D5)/UND(2)-OVD(D2^2*D4^2)/UND(8*D5)+OVD(D2*D4*(D3+D4))/UND(2)</td>	<td>mm³</td>	<td>in³</td>	<td>=EQS(D29,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$52_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Z1b =</td>	<td>=OVD(D4^2*D2)/UND(4)+D5*D3*(D4+D3-OVD(D5*D3)/UND(D2))</td>	<td>mm³</td>	<td>in³</td>	<td>=EQS(D31,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$54_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Z1 =</td>	<td>=IF(2*D5*D3<=D2*D4,D29,D31)</td>	<td>mm³</td>	<td>in³</td>	<td>=EQS(D33,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$56_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>s1 =</td>	<td>=(D2*D4/2*D5+D3)/2</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D35,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$58_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>s2 =</td>	<td>=D5*D3/D2+D4/2</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D37,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$60_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>s =</td>	<td>=IF(2*D5*D3<=D2*D4,D35,D37)</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D39,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$62_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Z2 =</td>	<td>=OVD(D2^2*D4)/UND(4)+D5*D3*(D2-D5)</td>	<td>mm³</td>	<td>in³</td>	<td>=EQS(D41,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$64_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Shape Factor</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>SF1 =</td>	<td>=OVD(D33*(D3+D4-D12))/UND(D18)</td>	<td></td>	<td></td>	<td>=EQS(D44,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$67_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>SF2 =</td>	<td>=OVD(D41*D2)/UND(2*D20)</td>	<td></td>	<td></td>	<td>=EQS(D46,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$69_0")</td></tr></tbody></table>

<table><tbody><tr><td></td>	<td>Length of sides</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>R =</td>	<td>20</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td>Ri =</td>	<td>15</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Area and distances from centroid to extremities</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Area</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>A =</td>	<td>=PI()*(D2^2-D3^2)</td>	<td>mm²</td>	<td>in²</td></tr>
				<tr><td></td>	<td>Distance to Extreme Fiber</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>yc =</td>	<td>=D2</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Moments and products of inertia and radii of gyration about central axes</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Moment of inertia</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Ix =</td>	<td>=(PI())/(4)*(D2^4-D3^4)</td>	<td>mm⁴</td>	<td>in⁴</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Iy =</td>	<td>=(PI())/(4)*(D2^4-D3^4)</td>	<td>mm⁴</td>	<td>in⁴</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Radius of gyration</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>rx =</td>	<td>=(1)/(2)*SQRT(D2^2+D3^2)</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>ry =</td>	<td>=(1)/(2)*SQRT(D2^2+D3^2)</td>	<td>mm</td>	<td>in</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Plastic section moduli, shape factors, and locations of plastic neutral axes</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Plastic section modulus</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Zx =</td>	<td>=1.333*(D2^3-D3^3)</td>	<td>mm³</td>	<td>in³</td></tr>
				<tr><td></td>	<td></td>	<td>Zy =</td>	<td>=1.333*(D2^3-D3^3)</td>	<td>mm³</td>	<td>in³</td></tr>
				<tr><td></td>	<td>Shape factor</td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>SFx =</td>	<td>=1.698*((D2^4-D3^3*D2)/(D2^4-D3^4))</td>	<td></td>	<td></td></tr></tbody></table>

<table><tbody><tr><td></td>	<td>Length of sides</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>R =</td>	<td>20</td>	<td>mm</td>	<td>in</td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Ri =</td>	<td>15</td>	<td>mm</td>	<td>in</td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Area and distances from centroid to extremities</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Area</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>A =</td>	<td>=PI()*(D2^2-D3^2)</td>	<td>mm²</td>	<td>in²</td>	<td>=EQS(D7,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$31_0")</td></tr>
				<tr><td></td>	<td>Distance to Extreme Fiber</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>yc =</td>	<td>=D2</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D9,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$33_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Moments and products of inertia and radii of gyration about central axes</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Moment of inertia</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Ix =</td>	<td>=OVD(PI())/UND(4)*(D2^4-D3^4)</td>	<td>mm⁴</td>	<td>in⁴</td>	<td>=EQS(D13,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$37_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Iy =</td>	<td>=OVD(PI())/UND(4)*(D2^4-D3^4)</td>	<td>mm⁴</td>	<td>in⁴</td>	<td>=EQS(D15,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$39_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Radius of gyration</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>rx =</td>	<td>=OVD(1)/UND(2)*SQRT(D2^2+D3^2)</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D18,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$42_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>ry =</td>	<td>=OVD(1)/UND(2)*SQRT(D2^2+D3^2)</td>	<td>mm</td>	<td>in</td>	<td>=EQS(D20,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$44_0")</td></tr>
				<tr><td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td>Plastic section moduli, shape factors, and locations of plastic neutral axes</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td>Plastic section modulus</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>Zx =</td>	<td>=1.333*(D2^3-D3^3)</td>	<td>mm³</td>	<td>in³</td>	<td>=EQS(D24,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$48_0")</td></tr>
				<tr><td></td>	<td></td>	<td>Zy =</td>	<td>=1.333*(D2^3-D3^3)</td>	<td>mm³</td>	<td>in³</td>	<td>=EQS(D25,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$49_0")</td></tr>
				<tr><td></td>	<td>Shape factor</td>	<td></td>	<td></td>	<td></td>	<td></td>	<td></td></tr>
				<tr><td></td>	<td></td>	<td>SFx =</td>	<td>=1.698*(OVD(D2^4-D3^3*D2)/UND(D2^4-D3^4))</td>	<td></td>	<td></td>	<td>=EQS(D27,"Units= ; EqnPrefix=Eqn. ; EqnNo= 0; Multiplication= 0; ShowWorking= 0; EqnStyle= 0; Eqp$H$51_0")</td></tr></tbody></table>

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