Hypersizer Stress Report

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Database Project Name Owner General Information C:\HyperSizer Data\Projects\Final Creation 7 zzzzzzz HyperSizer Admin Owner Creation Date Modification Date Assembly 1 Default assembly Report Summary HyperSizer Admin Sunday, April 26, 2015 at 2:48:30 PM Wednesday, April 29, 2015 at 2:41:06 PM Contents Assembly Report Number of Active Load Cases 4 Controlling load case 100 Controlling component 112:Upper Surface Panel Bay 12 Controlling failure mode Panel BucklingEnergy SolutionAll BC Lowest marginofsafety (MS) 0.0000047 Run Time (hh:mm:ss) 00:02:49 Weight Total (lbm) 1071 Beam, Unit Weight (lb / ft) 0 Beam, Total Length (ft) 0 Last Run Summary Beam, Total Length (ft) 0 Beam, Total Weight (lbm) 0 Panel, Unit Weight (lb / ft 2 ) 3.346 Panel, Total Area (ft 2 ) 320 Panel, Total Weight (lbm) 1071 Controlling Failure Mode, Strength (lbm) 212.4 Controlling Failure Mode, Buckling (lbm) 858.2 Controlling Failure Mode, Local Buckling (lbm) 0 Controlling Failure Mode, Minimum Gage (lbm) 0 Controlling Failure Mode, Negative Margin Structure (lbm) 0 R D k Finite Element Model Filenames Run Deck 1 FEM Filename

description

A technical report from Hypersizer.

Transcript of Hypersizer Stress Report

Page 1: Hypersizer Stress Report

Database

Project Name

Owner

General InformationC:\HyperSizer Data\Projects\Final Creation 7

zzzzzzz

HyperSizer AdminOwner

Creation Date

Modification Date

Assembly 1 Default assembly

Report Summary

HyperSizer Admin

Sunday, April 26, 2015 at 2:48:30 PM

Wednesday, April 29, 2015 at 2:41:06 PM

Contents Assembly Report

Number of Active Load Cases 4

Controlling load case 100

Controlling component  112:Upper Surface Panel Bay 12

Controlling failure mode Panel Buckling‐ Energy Solution‐ All BC

Lowest margin‐of‐safety (MS) 0.0000047

Run Time (hh:mm:ss) 00:02:49

Weight Total (lbm) 1071

    Beam, Unit Weight (lb / ft) 0

    Beam, Total Length (ft) 0

Last Run Summary

    Beam, Total Length (ft) 0

    Beam, Total Weight (lbm) 0

    Panel, Unit Weight (lb / ft2) 3.346

    Panel, Total Area (ft2) 320

    Panel, Total Weight (lbm) 1071

Controlling Failure Mode, Strength (lbm) 212.4

Controlling Failure Mode, Buckling (lbm) 858.2g g ( )

Controlling Failure Mode, Local Buckling (lbm) 0

Controlling Failure Mode, Minimum Gage (lbm) 0

Controlling Failure Mode, Negative Margin Structure (lbm) 0

R D k

Finite Element Model FilenamesRun Deck

1 FEM Filename

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FEA Force Filename

Temperature Fahrenheit (°F)

Length (Area) Inches (in)

M P d (lb )

FEM Units

Mass Pounds (lbm)

Force Pounds (lb)

Temperature °F

Weight lbm

Project Units

Weight lbm

Length in

Unit Weight (Panel, Area) lb / ft2

Unit Weight (Beam, Length) lb / ft

Force lb

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.1.hdb

C:\Users\Topaz_Wolf\Desktop\WB15_tech1_c27.bdf

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C:\Users\Topaz_Wolf\Desktop\WB15_tech1_c27.op2

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Assembly Area

(ft2)

UW Area

(lb / ft2)

Length

(in)

UW Length

(lb / ft)

Weight

(lbm)

% Total Weight

1 "Default assembly" 320 3.346 0 0 1071 100.00%

Totals 320 3.346 0 0 1071

Assembly Weight Summary

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Component Area

(ft2)

Unit Weight

(lb / ft2)

Weight

(lbm)

Lowest

MS

Controlling

Load Case

Lim/Ult

101 "Upper Surface Panel Bay 01" 61.17 5.877 359.5 0.0011 100 Ultimate

102 "Upper Surface Panel Bay 02" 17.67 3.692 65.24 0.076 100 Ultimate

103 "Upper Surface Panel Bay 03" 10.43 6.681 69.7 0.037 100 Ultimate

104 "Upper Surface Panel Bay 04" 15.71 2.263 35.56 0.21 100 Ultimate

105 "Upper Surface Panel Bay 05" 15.25 2.263 34.51 0.14 100 Ultimate

106 "Upper Surface Panel Bay 06" 14.41 2.263 32.61 0.066 100 Ultimate

107 "Upper Surface Panel Bay 07" 14.3 2.77 39.61 0.17 100 Ultimate

108 "Upper Surface Panel Bay 08" 13.88 7.305 101.4 0.014 100 Ultimate

109 "Upper Surface Panel Bay 09" 13.06 2.77 36.18 0.23 100 Ultimate

110 "Upper Surface Panel Bay 10" 12.02 2.263 27.21 0.16 100 Ultimate

111 "Upper Surface Panel Bay 11" 13.2 2.263 29.87 0.02 100 Ultimate

112 "Upper Surface Panel Bay 12" 11.86 6.517 77.32 4.66E‐06 100 Ultimate

113 "Upper Surface Panel Bay 13" 11.92 2.294 27.36 0.023 100 Limit

114 "Upper Surface Panel Bay 14" 11.27 1.787 20.14 0.073 100 Ultimate

115 "Upper Surface Panel Bay 15" 10.23 1.787 18.28 0.27 100 Ultimate

116 "Upper Surface Panel Bay 16" 9.796 1.787 17.51 0.11 100 Limit

117 "Upper Surface Panel Bay 17" 9.328 1.787 16.67 0.42 100 Limit

118 "Upper Surface Panel Bay 18" 8.204 1.787 14.66 0.99 100 Ultimate

119 "Upper Surface Panel Bay 19" 8.046 1.787 14.38 1.4 100 Ultimate

120 "Upper Surface Panel Bay 20" 7.387 1.311 9.686 0.14 100 Ultimate

121 "Upper Surface Panel Bay 21" 6.371 0.8352 5.321 0.044 100 Ultimate

122 "Upper Surface Panel Bay 22" 5.998 0.8352 5.01 0.53 100 Ultimate

123 "Upper Surface Panel Bay 23" 4.884 0.8352 4.079 1.3 100 Ultimate

124 "Upper Surface Panel Bay 24" 4.364 0.8352 3.645 3 100 Ultimate

125 "Upper Surface Panel Bay 25" 3.223 0.8044 2.592 0.23 100 Ultimate

126 "Upper Surface Panel Bay 26" 3.556 0.4925 1.751 0.46 100 Ultimate

127 "Upper Surface Panel Bay 27" 2.422 0.3283 0.7951 3.3 100 Ultimate

Totals 320 3.346 1071

Component Panel Weight Summary

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AID Controlling

Failure Mode

11 Panel Buckling, Energy Solution, All BC

11 Panel Buckling, Energy Solution, All BC

11 Panel Buckling, Energy Solution, All BC

11 Panel Buckling, Energy Solution, All BC

11 Panel Buckling, Energy Solution, All BC

11 Panel Buckling, Energy Solution, All BC

142 Composite Strength, Tsai‐Wu Interaction

11 Panel Buckling, Energy Solution, All BC

142 Composite Strength, Tsai‐Wu Interaction

11 Panel Buckling, Energy Solution, All BC

11 Panel Buckling, Energy Solution, All BC

11 Panel Buckling, Energy Solution, All BC

104 Sandwich Flatwise Tension w/ Interlaminar Shear Interaction

11 Panel Buckling, Energy Solution, All BC

142 Composite Strength, Tsai‐Wu Interaction

104 Sandwich Flatwise Tension w/ Interlaminar Shear Interaction

104 Sandwich Flatwise Tension w/ Interlaminar Shear Interaction

142 Composite Strength, Tsai‐Wu Interaction

142 Composite Strength, Tsai‐Wu Interaction

142 Composite Strength, Tsai‐Wu Interaction

142 Composite Strength, Tsai‐Wu Interaction

142 Composite Strength, Tsai‐Wu Interaction

143 Composite Strength, Tsai‐Hahn Interaction

143 Composite Strength, Tsai‐Hahn Interaction

11 Panel Buckling, Energy Solution, All BC

11 Panel Buckling, Energy Solution, All BC

11 Panel Buckling, Energy Solution, All BC

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Comp.

ID

T

(in)

Unit Wt.

(lb / ft2)

Area

(ft2)

Wt.

(lbm)

Component Dimensions

ID (in) (lb / ft ) (ft ) (lbm)

101 0.716 5.877 61.17 359.5

108 0.89 7.305 13.88 101.4

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Stack Material

[EL] Effective Laminates "(21% 0, 60% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine (1)", Form: 

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

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Hybrid (40% Fabric), Dry

brid (40% Fabric), Dry

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Comp. Ttop Tbottom Height Unit Wt. Area Wt.

Component DimensionsComp.

ID

Ttop(in)

Tbottom(in)

Height

(in)

Unit Wt.

(lb / ft2)

Area

(ft2)

Wt.

(lbm)

112 0.02 0.774 0.794 6.517 11.86 77.32

125 0.078 0.02 0.098 0.8044 3.223 2.592

127 0.02 0.02 0.04 0.3283 2.422 0.7951

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Top Stack MaterialTop Stack Material

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(21% 0, 40% 45, 39% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

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Bottom Stack MaterialBottom Stack Material

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(21% 0, 40% 45, 39% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

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brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry

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Comp.

ID

Ttop(in)

Tmiddle

(in)

Tbottom(in)

Height

(in)

Unit Wt.

(lb / ft2)

Area

(ft2)

Wt.

(lbm)

103 0.02 0.484 0.31 0.814 6.681 10.43 69.7

126 0.02 0.02 0.02 0.06 0.4925 3.556 1.751

Component Dimensions

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Top Stack Material

[EL] Effective Laminates "(21% 0, 60% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine (1)", Form: 

[EL] Effective Laminates "(21% 0, 60% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine (1)", Form: 

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Middle Stack Material

[EL] Effective Laminates "(21% 0, 60% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine (1)", Form: 

[EL] Effective Laminates "(21% 0, 60% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine (1)", Form: 

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Bottom Stack Material

[EL] Effective Laminates "(21% 0, 60% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine (1)", Form: 

[EL] Effective Laminates "(21% 0, 60% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine (1)", Form: 

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Hybrid (40% Fabric), Dry

Hybrid (40% Fabric), Dry

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Comp.

ID

Ttop face(in)

Tcore(in)

Tbottom face

(in)

Height

(in)

Unit Wt.

(lb / ft2)

Area

(ft2)

Wt.

(lbm)

Component Dimensions

ID (in) (in) (in) (in) (lb / ft ) (ft ) (lbm)

102 0.194 1 0.194 1.388 3.692 17.67 65.24

104 0.078 1 0.136 1.214 2.263 15.71 35.56

105 0.078 1 0.136 1.214 2.263 15.25 34.51

106 0.078 1 0.136 1.214 2.263 14.41 32.61

107 0.078 2 0.136 2.214 2.77 14.3 39.61

109 0.078 2 0.136 2.214 2.77 13.06 36.18

110 0.078 1 0.136 1.214 2.263 12.02 27.21

111 0.078 1 0.136 1.214 2.263 13.2 29.87

113 0.078 2 0.078 2.156 2.294 11.92 27.36

114 0.078 1 0.078 1.156 1.787 11.27 20.14

115 0.078 1 0.078 1.156 1.787 10.23 18.28

116 0.078 1 0.078 1.156 1.787 9.796 17.51

117 0 078 1 0 078 1 156 1 787 9 328 16 67117 0.078 1 0.078 1.156 1.787 9.328 16.67

118 0.078 1 0.078 1.156 1.787 8.204 14.66

119 0.078 1 0.078 1.156 1.787 8.046 14.38

120 0.02 1 0.078 1.098 1.311 7.387 9.686

121 0.02 1 0.02 1.04 0.8352 6.371 5.321

122 0.02 1 0.02 1.04 0.8352 5.998 5.01

123 0.02 1 0.02 1.04 0.8352 4.884 4.079

124 0.02 1 0.02 1.04 0.8352 4.364 3.645

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Top Face Material

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0 40% 45 19% 90) AS4/3502 Tape Pristine / AS4/3501 6 Fabric Pristine" Form: Hyb[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb[ ] ( , , ) / p / / , y

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

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Core Material

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6 1 pcf 1/8 5052 0015" Density 0 00352 DryHexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dryp / , y , y

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

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Bottom Face Material

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0 40% 45 19% 90) AS4/3502 Tape Pristine / AS4/3501 6 Fabric Pristine" Form: Hyb[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb[ ] ( , , ) / p / / , y

[EL] Effective Laminates "(41% 0, 40% 45, 19% 90) AS4/3502 Tape Pristine / AS4/3501‐6 Fabric Pristine", Form: Hyb

Page 24: Hypersizer Stress Report

brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric) Drybrid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry

brid (40% Fabric), Dry( ), y

brid (40% Fabric), Dry

Page 25: Hypersizer Stress Report

Family Hexcel

Owner CRD

Created

Last Modified

*Density 0.00352 (lb/in3)

*Wet DRY

Form NONE

Specification NONE

Cell Size 0.125 (in)

Manufacturer Hexcell

Description

Temperature

(°F)

Tension, *Et

(Msi)

Compression, *Ec

(Msi)

Shear (Trans\W), *Gw

(Msi)

72 0.24 0.24 0.041

Temperature

(°F)

Tension, *Ftu

(ksi)

Shear (Trans\W), *Fsuw

(ksi)

Shear (L\Ribbon), *Fsul

(ksi)

72 0.68 0.272 0.455

Temperature

(°F)

Thermal Conductivity

Longitudinal, Kl

(B‐ft/ft2/hr/F)

Thermal Conductivity

Transverse, Kw

(B‐ft/ft2/hr/F)

Thermal Conductivity

Thickness, Kt

(B‐ft/ft2/hr/F)

72

Temperature Dependent Properties, Stiffness

Temperature Dependent Properties, Stress Allowables

Temperature Dependent Properties, Thermal

Hexcel "Hexcel 6.1 pcf 1/8‐5052‐.0015", Density 0.00352, Dry

Saturday, January 10, 1998 at 3:34:00 PM

Wednesday, April 25, 2012 at 5:26:39 PM

Hexcell 5052 Alloy Hexagonal Aluminum Honeycomb

Material Summary (name and * fields determine unique material)

Page 26: Hypersizer Stress Report

Shear (L\Ribbon), *Gl

(Msi)

*SScfl at 0.5" *SScfh at 1.5"

0.098 1.05 0.85

Stabilized, *Fcus

(ksi)

Bare, *Fcub

(ksi)

Crush, *Fcuc

(ksi)

0.68 0.65 0.45

Specific Heat

C

(B/lb/F)