17,005 Documents in our Technical Library
2458406 Total Downloads

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 ...

AA-SM-026-005

AA-SM-026-005
  • Version
  • 1002 Downloads
  • 109.79 KB File Size
  • 1 File Count
  • September 18, 2016 Create Date
  • September 18, 2016 Last Updated
Scroll for Details

AA-SM-026-005 Beam Analysis - Cantilever - Triangular load Whole 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-026-005

 

FileAction
AA-SM-026-005 Beam Analysis - Cantilever - Triangle load Whole Span Peak at Support.xlsxDownload 

Comment On This Post

Your email address will not be published. Required fields are marked *

AA-SM-026-005

AA-SM-026-005
  • Version
  • 1002 Downloads
  • 109.79 KB File Size
  • 1 File Count
  • September 18, 2016 Create Date
  • September 18, 2016 Last Updated
Scroll for Details

AA-SM-026-005 Beam Analysis - Cantilever - Triangular load Whole 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-026-005

 

FileAction
AA-SM-026-005 Beam Analysis - Cantilever - Triangle load Whole Span Peak at Support.xlsxDownload 
17,005 Documents in our Technical Library
2458406 Total Downloads

Search The Technical Library

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 ...