Technical Data

 

Pro Seam Panels properties

 

 

SECTION PROPERTIES

 

 

 

 

 

 

 

TOP FLAT IN

COMPRESSION

BOTTOM FLAT IN

COMPRESSION

 Ga

Fy

(KSI)

Fb

(KSI)

WEIGHT

(PSF)

GIRTH

(in.)

Ix

(in4/ft)

Sx

(in3/ft)

Ix

(in4/ft)

Sx

(in3/ft)

26

50.0

30.0

1.13

30.0

.2714

.1191

.1020

.0648

24

50.0

30.0

1.44

30.0

.3559

.1490

.1453

.0961

22

50.0

30.0

1.75

30.0

.4367

.1825

.1920

.1312

 

 

 

Load In (stress)

Load In (deflection)

Ga

Span

3

3.5

4

4.5

5

5.5

6

6.5

7

7.5

3

3.5

4

4.5

5

5.5

6

6.5

7

7.5

26

Simple

264

194

148

117

95

78

66

56

48

42

264

194

148

117

95

78

66

56

48

42

24

Simple

331

243

186

147

119

98

82

70

60

53

331

243

186

147

119

98

82

70

60

53

26

Two

129

95

72

57

46

38

32

27

23

20

129

95

72

57

46

38

32

27

23

20

24

Two

213

156

120

94

76

63

53

45

39

34

213

156

120

94

76

63

53

45

39

34

26

Three +

162

119

91

72

58

48

40

34

29

26

162

119

91

72

58

48

40

34

29

26

24

Three +

268

196

150

119

96

79

67

57

49

42

268

196

150

119

96

79

67

57

49

42

 

 

 

Load Out (stress)

Load Out (deflection)

Ga

Span

3

3.5

4

4.5

5

5.5

6

6.5

7

7.5

3

3.5

4

4.5

5

5.5

6

6.5

7

7.5

26

Simple

129

95

72

57

46

38

32

27

23

20

129

95

72

57

46

38

32

25

20

16

24

Simple

213

156

120

94

76

63

53

45

39

34

213

156

120

94

76

60

46

36

29

23

26

Two

264

194

148

117

95

78

66

56

48

42

264

194

148

117

95

78

66

56

47

38

24

Two

331

243

186

147

119

98

82

70

60

53

331

243

186

147

119

98

82

70

60

53

26

Three +

332

244

186

147

119

98

83

70

61

53

332

244

186

140

102

77

59

46

37

30

24

Three +

415

305

233

184

149

123

103

88

76

66

415

305

233

184

146

109

84

66

53

43

NOTES:

1.     Stress loads are total loads limited by maximum bending stresses based on calculated properties
2.     Deflection loads are limited by a maximum deflection ratio of L/240 or the maximum bending stress.
3.     To obtain uplift loads due to wind, multiply tabulated values by 1.333.
4.     All panels are Fy = 50 KSI.
5.     All calculations for the properties of Pro Seam panels are calculated in accordance with the 1968 edition of Specifications for the Design of Light Gauge Cold Formed Steel Structural Members, published by the American Iron and Steel Institute (AISI).

All steel substrates are manufactured in accordance to ASTM A446 Specifications.  Protective coatings shall be either Galvanized G90, 1.25 oz/sq. ft., meeting ASTM A525; or Galvalume AZ55, .55 oz/sq. ft., meeting ASTM A792 Specifications.

 

Rib-12 Panel Properties

SECTION PROPERTIES

80,000 psi

 

Load In

Load Out

Gauge

Ix

(in4/ft)

Sx

(in3/ft)

Ma

(k-in)

Ix

(in4/ft)

Sx

(in3/ft)

Ma

(k-in)

28

0.0222

0.0218

3.139

0.0241

0.0387

5.577

 

26

0.0294

0.0293

4.223

0.0371

0.0500

7.195

 

24

0.0465

0.0481

6.924

0.0520

0.0671

9.659

 

22

0.0647

0.0689

9.919

0.0676

0.0842

12.127

 

 

SECTION PROPERTIES

50,000 psi

 

Load In

Load Out

Gauge

 

 

Sx

(in3/ft)

Ma

(k-in)

Ix

(in4/ft)

Sx

(in3/ft)

Ma

(k-in)

24

0.0547

0.0589

5.299

0.0542

0.0677

6.089

 

22

0.0737

0.0811

7.298

0.0704

0.0849

7.645

 

1.  Section properties are calculated in accordance with the 1986 AISI Cold Formed Steel Design Manual, 1989 Addendums.
2.  Section properties are based on base material thickness without protective coatings.
3.  Panels with purlin bearings legs are available in Rib-12 Galvalume™ only.
4.  All steel substrates are manufactured in accordance to ASTM A446 specifications.  Protective metallic coatings shall be galvanized, G90, 1.25 oz/sf, meeting ASTM A525 or Galvalume™, AZ55, 0.55 oz/sf, meeting ASTM A792 specifications.
5.  Organic paint coatings shall be silicone polyester equal to Ceram-A-Star™ 950 and shall meet ASTM G23, G26 and B117.

80,000 psi

SIMPLE SPAN

 

Load Out (stress)

Load Out (deflection)

Ga

3’

4’

5’

6’

7’

3’

4’

5’

6’

7’

28

103

58

37

26

19

201

91

51

31

21

26

139

78

50

35

26

294

127

66

39

25

24

228

128

82

57

42

413

179

96

57

36

22

327

184

118

82

60

54

240

125

74

47

TWO SPAN

28

103

58

37

26

19

201

91

51

31

20

26

139

78

50

35

26

294

127

66

39

25

24

228

128

82

57

42

413

179

96

57

36

22

327

184

118

82

60

554

240

125

74

47

THREE SPAN

28

129

73

47

32

24

183

83

45

26

17

26

174

88

63

44

32

240

134

56

33

21

24

285

160

103

71

52

348

151

79

46

30

22

408

230

147

102

75

453

195

102

59

37

 

80,000 psi

SIMPLE SPAN

 

Load In (stress)

Load In (deflection)

Ga

3’

4’

5’

6’

7’

3’

4’

5’

6’

7’

28

76

44

28

19

14

88

41

23

14

10

26

104

59

38

26

19

119

55

33

19

12

24

171

96

62

43

31

203

86

44

25

16

22

245

138

88

61

45

252

106

54

32

20

TWO SPAN

28

184

103

66

46

34

189

89

49

30

20

26

237

133

85

59

44

258

121

67

41

29

24

318

179

115

89

58

417

206

105

61

38

22

399

225

144

100

73

607

256

131

76

48

THREE SPAN

28

121

68

44

30

22

154

72

40

25

16

26

163

92

59

41

30

211

98

54

36

23

24

267

105

96

67

49

339

161

83

48

30

22

374

211

135

94

69

475

201

103

59

37

 

Zee Properties

 

 

 

PROPERTIES OF FULL SECTION

Effec. Sec. Prop.

 

 

 

Axis x - x

Axis y - y

 

 

 

 

 

 

 

G

Area

 

Ix

Sx

rx

Iy

Sy

ry

Ixy

J

Cw

ro

Ix

Sx

Ma

a

In.

#/In.

In4

In3

In.

In4

In3

In.

In.

In4

In6

In.

In4

In3

Kip-in.

16

.844

2.869

8.120

2.030

3.102

1.221

.414

1.203

2.385

.001006

12.437

3.327

7.271

1.699

55.951

15

.948

3.223

9.099

2.275

3.098

1.365

.463

1.200

2.673

.001431

13.831

3.322

8.317

1.971

64.913

14

1.050

3.571

10.058

2.514

3.095

1.504

.511

1.197

2.955

.001954

15.173

3.318

  9.210

2.185

  71.955

12

1.460

4.964

13.847

3.462

3.080

2.048

.699

1.184

4.072

.005325

20.255

3.300

13.564

3.344

110.141

1.  Section properties are calculated in accordance with the 1986 AISI Cold-Formed Steel Design Manual 1989 Addendum.
2.  Minimum yield strength of steel is 55,000 psi (galvanized members are 50,000 psi min.).

 

Cee Properties

 

 

 

PROPERTIES OF FULL SECTION

 

 

 

Axis x - x

Axis y - y

 

Area

 

Ix

Sx

rx

Iy

Sy

ry

X

Ga

In2

#/Ft

In4

In3

In.

In4

In3

In.

In.

CEE

16

0.830

2.824

  7.862

1.966

3.077

0.674

0.370

0.901

0.679

15

0.932

3.169

  8.801

2.200

3.073

0.750

0.412

0.897

0.679

14

1.032

3.509

  9.716

2.429

3.068

0.824

0.453

0.894

0.679

12

1.430

4.861

13.311

3.328

3.051

1.104

0.607

0.879

0.681

EAVE STRUT

14

1.405

4.779

15.581

3.895

3.330

4.526

1.351

1.795

1.649

 

 

PROPERTIES OF FULL SECTION

Effec. Sec. Prop.

 

m

J

Cw

j

ro

xo

Ix

Sx

Ma

Ga

In.

In4

In6

In.

In.

In.

In4

In3

Kin-in.

CEE

16

1.131

0.000990

8.977

4.520

3.667

-1.780

7.200

1.706

56.186

15

1.127

0.001407

9.977

4.524

3.659

-1.772

8.071

1.917

63.142

14

1.123

0.001919

10.938

4.528

3.651

-1.765

9.144

2.203

72.541

12

1.108

0.005215

14.565

4.547

3.619

-1.736

13.171

3.268

107.641

EAVE STRUT

14

2.349

0.002614

57.441

5.627

5.477

-3.961

11.708

2.480

81.667

1.  Section properties are calculated in accordance with the 1986 AISI Cold-Formed Steel Design Manual 1989 Addendum.
2.  Minimum yield strength of steel is 55,000 psi (galvanized members are 50,000 psi min.).

 

Bracing Properties


Bracing to be AN1265 strap attached to bottom of purlins with either #14 self-tapper or #12 self-drilling screw.