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AA-CP-20212-001
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ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
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AA-SM-101-025

  • Version
  • 1995 Downloads
  • 305.27 KB File Size
  • 3 File Count
  • January 5, 2017 Create Date
  • January 5, 2017 Last Updated
Scroll for Details

AA-SM-101-025 Bolt Pull Through Failure Load in Laminate

Free Engineering Spreadsheets: Pull-Through Method, defined in "Pull Through Failure of Bolted Composite Joints". Note that the spreadsheet cells with blue ink are the input values - all other cells are either text or values generated by the spreadsheet.

 


28 July 2017 - Rev B Uploaded - Corrected parameter for Fastener Head Diameter

5 January 2017 - Rev A uploaded, added link to specific technical reference data

FileAction
AA-SM-101-025 Bolt Pull Through Failure Load in Laminate Rev B.xlsxDownload 
AA-SM-101-025 Bolt Pull Through Failure Load in Laminate Rev A.xlsxDownload 
AA-SM-101-025 Bolt Pull Through Failure Load in Laminate.xlsxDownload 

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AA-SM-101-025

  • Version
  • 1995 Downloads
  • 305.27 KB File Size
  • 3 File Count
  • January 5, 2017 Create Date
  • January 5, 2017 Last Updated
Scroll for Details

AA-SM-101-025 Bolt Pull Through Failure Load in Laminate

Free Engineering Spreadsheets: Pull-Through Method, defined in "Pull Through Failure of Bolted Composite Joints". Note that the spreadsheet cells with blue ink are the input values - all other cells are either text or values generated by the spreadsheet.

 


28 July 2017 - Rev B Uploaded - Corrected parameter for Fastener Head Diameter

5 January 2017 - Rev A uploaded, added link to specific technical reference data

FileAction
AA-SM-101-025 Bolt Pull Through Failure Load in Laminate Rev B.xlsxDownload 
AA-SM-101-025 Bolt Pull Through Failure Load in Laminate Rev A.xlsxDownload 
AA-SM-101-025 Bolt Pull Through Failure Load in Laminate.xlsxDownload 
17,005 Documents in our Technical Library
2627925 Total Downloads

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Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...