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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 ...
MIL-R-7885D General Specification for Rivets, Blind, Structural, Mechanically Locked Spindle and Friction Locked Spindle
This specification covers mechanically locked spindle and  friction locked spindle ...

AA-SM-026-006

AA-SM-026-006
  • Version
  • 840 Downloads
  • 109.57 KB File Size
  • 2 File Count
  • September 18, 2016 Create Date
  • January 16, 2022 Last Updated
Scroll for Details

AA-SM-026-006 Beam Analysis - Cantilever - Triangular load Part Span Peak at Support

Free Engineering Spreadsheets: Beam analysis spreadsheet, based on the method in NASA-TM-73305, the NASA Stress Analysis Manual. Note that the spreadsheet cells with blue ink are the input values - all other cells are either text or values generated by the spreadsheet.

aa-sm-026-006

 


16 January 2022 - Rev A added, corrected peak moment calculation and sign of theta at point D

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FileAction
AA-SM-026-006 Beam Analysis - Cantilever - Triangle load Part Span Peak at Support - Rev A.xlsxDownload 
AA-SM-026-006 Beam Analysis - Cantilever - Triangle load Part Span Peak at Support.xlsxDownload 

AA-SM-026-006

AA-SM-026-006
  • Version
  • 840 Downloads
  • 109.57 KB File Size
  • 2 File Count
  • September 18, 2016 Create Date
  • January 16, 2022 Last Updated
Scroll for Details

AA-SM-026-006 Beam Analysis - Cantilever - Triangular load Part Span Peak at Support

Free Engineering Spreadsheets: Beam analysis spreadsheet, based on the method in NASA-TM-73305, the NASA Stress Analysis Manual. Note that the spreadsheet cells with blue ink are the input values - all other cells are either text or values generated by the spreadsheet.

aa-sm-026-006

 


16 January 2022 - Rev A added, corrected peak moment calculation and sign of theta at point D

FileAction
AA-SM-026-006 Beam Analysis - Cantilever - Triangle load Part Span Peak at Support - Rev A.xlsxDownload 
AA-SM-026-006 Beam Analysis - Cantilever - Triangle load Part Span Peak at Support.xlsxDownload 
17,004 Documents in our Technical Library
2130390 Total Downloads

Search The Technical Library

Newest Additions

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 ...
MIL-R-7885D General Specification for Rivets, Blind, Structural, Mechanically Locked Spindle and Friction Locked Spindle
This specification covers mechanically locked spindle and  friction locked spindle ...