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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-002-011

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  • 831 Downloads
  • 0.00 KB File Size
  • 1 File Count
  • June 10, 2017 Create Date
  • June 10, 2017 Last Updated
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AA-SM-002-011 Torsion - Regular Sections - Solid Round Rod

Free spreadsheet analysis tool to calculate the peak shear stress and angular deflection of a solid regular cross section of a finite-length rod/bar, given the cross-section, length and shear modulus, Based on methods in NASA TM-X-73306 and AFFDL-TR-69-42.

 

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AA-SM-002-011

  • Version
  • 831 Downloads
  • 0.00 KB File Size
  • 1 File Count
  • June 10, 2017 Create Date
  • June 10, 2017 Last Updated
Scroll for Details

AA-SM-002-011 Torsion - Regular Sections - Solid Round Rod

Free spreadsheet analysis tool to calculate the peak shear stress and angular deflection of a solid regular cross section of a finite-length rod/bar, given the cross-section, length and shear modulus, Based on methods in NASA TM-X-73306 and AFFDL-TR-69-42.

 

FileAction
AA-SM-002-011 Torsion - Regular Sections - Solid Round Rod.xlsxDownload 
17,005 Documents in our Technical Library
2492526 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 ...