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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-009-005

AA-SM-009-005
  • Version
  • 2914 Downloads
  • 348.62 KB File Size
  • 3 File Count
  • March 2, 2016 Create Date
  • March 2, 2016 Last Updated
Scroll for Details

AA-SM-009-005 Lug Analysis - Compact Oblique

Free Engineering Spreadsheets: Lug Analysis - Compact Oblique. 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-009-005

 


19 April 2016 - Updated: Shear Bearing allowable now calculated using the longitudinal (not the transverse) material strength

31 August 2016 - Rev A added, added links and included general corrections and improvements

27 June 2017 - Rev B added, corrected the Kt generation for the axial failure

FileAction
AA-SM-009-005 Lug Analysis - Compact Oblique - Rev B.xlsxDownload 
AA-SM-009-005 Lug Analysis - Compact Oblique - Rev A.xlsxDownload 
1461077390wpdm_AA-SM-009-005 Lug Analysis - Compact Oblique.xlsxDownload 

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AA-SM-009-005

AA-SM-009-005
  • Version
  • 2914 Downloads
  • 348.62 KB File Size
  • 3 File Count
  • March 2, 2016 Create Date
  • March 2, 2016 Last Updated
Scroll for Details

AA-SM-009-005 Lug Analysis - Compact Oblique

Free Engineering Spreadsheets: Lug Analysis - Compact Oblique. 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-009-005

 


19 April 2016 - Updated: Shear Bearing allowable now calculated using the longitudinal (not the transverse) material strength

31 August 2016 - Rev A added, added links and included general corrections and improvements

27 June 2017 - Rev B added, corrected the Kt generation for the axial failure

FileAction
AA-SM-009-005 Lug Analysis - Compact Oblique - Rev B.xlsxDownload 
AA-SM-009-005 Lug Analysis - Compact Oblique - Rev A.xlsxDownload 
1461077390wpdm_AA-SM-009-005 Lug Analysis - Compact Oblique.xlsxDownload 
17,005 Documents in our Technical Library
2500277 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 ...