REVOLVED CIRCLE SECTIONS. Triangle revolved about its Centroid

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REVOLVED CIRCLE SECTIONS Triangle revolved about its Centroid Box-in Method Circle Sector Method Integrating to solve I, Ax, and A for a revolved triangle is difficult. A quadrilateral and another triangle are created above and below the centroid as the triangle in question is rotated. By drawing a rectangle around the triangle and dividing the figures along the altitude, the values of the right triangles with respect to the rectangles can be resolved. The quantities I, Ax, and A required for engineering calculations may be determined for any circular sector (refer to Circle Section Integrals). Subtracting the rotated sector values of interest from the circle values leaves only the triangle related quantities. The centroid of the triangle with respect to the circle center is easily calculated, making this the preferred method. Maximum loads for multiple log beams with allowance for the scribe, or ridges with irregular pitches, may be estimated with relative ease using circle sectors.

REVOLVED CIRCLE SECTIONS Triangle revolved about its Centroid Sample Calculation C Circle centerline 16.26020 R = 5 8 10 Reference Axis I SEMI-CIRCLE = 25.3693 I TRIANGLE = 25.3693 (119.81007 + 33.6706) = 92.1598 Note : Most calculations return I TRIANGLE = I ± Ar 2 at this stage and require further work (see example below). The angle of revolution in this case places the median, and hence the centroid of the triangle, on the circle centerline. Thus, 92.16 is the final result. A 6 Sector A A = 11.18238 x = 3.81553 r = 3.0522 I X = 37.88988 I Y = 3.0909 I R + Ar 2 = 119.81007 Sector B A =.08753 x =.036 r = 2.6218 I X = 7.570 I Y =.28153 I R + Ar 2 = 33.6706 Sector C A = 39.26991 x = 2.12207 r =.5918 I X = 25.3693 I Y = 68.59810 I R + Ar 2 = 25.3698 Triangle A = 2 h =.8 x = 1.6 r = zero Calculations with respect to the Reference Axis: I + Ar 2 I CIRCLE = 25.36926 I A = 70.70277 I B = 27.6551 I C = 993.85073 I TRIANGLE = I CIRCLE (I A +I B +I C ) = 692.16035 I TRIANGLE about its centroid: I Ar 2 = 692.16053 2 (5) 2 = 92.16053 B 53.13010 36.86990

REVOLVED CIRCLE SECTIONS Ridge Beam: Second Moment of Area Sample Calculation 9 / 12 Pitch 36.86990 8 / 12 Pitch 33.69007.51519 53.13010 56.30993 Neutral Axis of Beam Centerline of Log 1 dia. 9 / 12 Side A = 8.01156 x = 6.16510 r =.93208 I X = 28.9927 I Y = 1.08153 I R = 11.12957 I R + Ar 2 = 206.0107 Initial Log Calculations A = 9π = 153.9380 I = 7 π / = 1885.7099 8 / 12 Side A = 6.19675 x = 6.29817 r = 5.2039 I X = 1 9.08178 I Y =.5899 I R = 6.2793 I R + Ar 2 = 176.526 Final Beam Calculations: Log values Sector values I BEAM, wrt Log center = 1885.7099 (176.526 +206.0107) = 1503.2728 A BEAM = 153.9380 (6.19675 + 8.01156) = 139.72973 First Moment of Area = 0 (32.7339 + 39.51365) = 71.9870 Centroid = 71.9870 139.72972 =.51519 (= 6.881 from bottom ) I BEAM = I (Ar 2 ) = 1503.2728 139.72972 (.51519) 2 = 166.18711 Taking the bottom edge of the log as a reference line yields the same result: I LOG I SECTORS = 928.7095 (93.72081 + 1151.77168) = 732.2126 I BEAM = I (Ar 2 ) = 732.2126 139.72792 (6.881) 2 = 166.19198

Circle: I = πd 6 Rectangle: I = bd 3 RECTANGULAR SECTION equivalent to a CIRCULAR SECTION 12 Setting the values of I equal, and the rectangle depth d = D: πd 6 bd 3 12 =, and b = 3πD 16 D = d Circle: A = πd 2 Rectangle: A = bd Substituting equivalent Circle values: Rectangle A = 3πD 2 b 16 Equating the values of I with d = D ensures both beams have equal resisting moments and deflections.* The distance from the neutral axis to the extreme fibre c is also equal for both sections. These conditions are satisfied if D = 3 32M π F b Comparing the two areas, the rectangle area is only 3 / of the area of the circle. The maximum shear stress of the circular section is 2 / 3 that of the equivalent rectangular section. * For a uniformly loaded beam, supported at the ends: F b I M r = Maximum deflection = c 5wl 38 EI

ANALYSIS of LOG SPAN TABLES FORMULAS Log Diameter from Bending Moment Formula Squaring the Circle Circle: A = Square: A = b 2 b = πd 2 πd 2 D b πd 2 = Section Modulus of a Square: S =, M = F b S = 6 b = 3 6M F b Substituting πd 2 for b gives the formula on page 7. πd 3 Section Modulus of a Circle: S =, F πd M = F b S = 3 b 32 32 D = 3 32M π F b 3 6M F b The Bending Moment limit formula on page 7, with the terms re-arranged. b 3 F b 3 b 6 The formula for a beam of square section, equivalent to the formula on page 68 when b = h Solving for D yields the formula for a circular section based on the section modulus. This equation disagrees with the Log Span Tables formula, which is based on the width b of a beam of square section that has an area equal to a circular cross section. The Log Span Tables version tends to return smaller log diameters. The following shear limit formula also compares cross sectional areas.

ANALYSIS of LOG SPAN TABLES FORMULAS Log Diameter from Shear Formula Re-arranging the shear limit formula on page 9: π D 2 = π D 2 6V F v = 6V F v, and dividing both sides of the equation by gives: = 3V 2F v The left hand term is the area of a circle. Reference for the following formulas: Mechanics of Materials, J. Lister Robinson, John Wiley & Sons, 1967, pages 96-97 Re-arranging the shear limit formula for a rectangle: The variables bh on the left side equal the area of a rectangle. Q is the First Moment of area above the Neutral Axis, for a Circle: Q = D 3 12 [ Rectangle: Q = bh 2 8 ] Circle width at the Neutral Axis: b = D [ Rectangle: b = b ] Circle Second Moment of Area: I = π D 6 [ Rectangle: I = bh 3 12 ] Substituting for the variables Q, b, and I for the circle in the general formula and solving for D gives: D = F 3V F v =, bh = 2bh F v = QV I b 16V 3π v 3V 2F v This is a general formula for maximum shear stress, regardless of the cross sectional geometry. This equation differs from the formula in the Log Span Tables. The Log Span Tables version returns larger log diameters. Substituting the appropriate rectangle variables in the general formula returns the standard equation F v = 3V 2bh, in accord with the Log Span Tables (page 70).

NOTES and REFERENCES Since measurements are with respect to the center of a circle, no distiction is made between moment arms x and y The quantity r denotes the moment arm y from the x - axis I X : Second Momemt of Area about the x - axis I Y : Second Momemt of Area about the y - axis I R : Second Momemt of Area revolved, with respect to the x - axis The Integrator at mathworld.wolfram.com returns the same integrals for A, Ax, and I as described in Circle Section Integrals. The Box-in and Circle Sector methods of calculation both return equal values for A, Ax and I and polar moment J of a triangle. Calculated centroids of triangles and log beam sections may be tested by making a lamina: The lamina will balance horizontally or level about the centroid. The lamina may be rotated to any position, provided the plane of the lamina is plumb, and the line of a plumb bob will pass through the centroid of the lamina. Reasonably accurate estimates of A, Ax, I, and F v for multiple log beams may be obtained by summation employing horizontal strips. Engineering values for circles representing log cross sections are calculated on the basis of bending moment, deflection and shear stress, without reference to equivalent rectangular or square sections. Log Span Tables B. Allan Mackie, Norman A. Read, Thomas M. Hahney 2000 Canada, pages as referenced above Mechanics of Materials J. Lister Robinson, John Wiley & Sons, 1967, pages 96-97