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NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
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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-026-013

  • Version
  • 2120 Downloads
  • 110.11 KB File Size
  • 2 File Count
  • November 10, 2016 Create Date
  • December 21, 2019 Last Updated
Scroll for Details

AA-SM-026-013 Beam Analysis - Simply Supported Both Ends - UDL along Entire Length

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-026-013


17 Jan 2017 - Rev A - X axis of Shear Force and Bending Moment diagram correct to give correct maximum value

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AA-SM-026-013 Beam Analysis - Simply Supported Both Ends - UDL along Entire Length - Rev A.xlsxDownload 
AA-SM-026-013 Beam Analysis - Simply Supported Both Ends - UDL along Entire Length.xlsxDownload 

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AA-SM-026-013

  • Version
  • 2120 Downloads
  • 110.11 KB File Size
  • 2 File Count
  • November 10, 2016 Create Date
  • December 21, 2019 Last Updated
Scroll for Details

AA-SM-026-013 Beam Analysis - Simply Supported Both Ends - UDL along Entire Length

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-026-013


17 Jan 2017 - Rev A - X axis of Shear Force and Bending Moment diagram correct to give correct maximum value

FileAction
AA-SM-026-013 Beam Analysis - Simply Supported Both Ends - UDL along Entire Length - Rev A.xlsxDownload 
AA-SM-026-013 Beam Analysis - Simply Supported Both Ends - UDL along Entire Length.xlsxDownload 
17,005 Documents in our Technical Library
2449313 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 ...