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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-515-000

  • Version
  • 2281 Downloads
  • 634.59 KB File Size
  • 2 File Count
  • March 13, 2016 Create Date
  • March 13, 2016 Last Updated
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AA-SM-515-000 Loads - Simplified Part 23 Aircraft Loads, Part 23 Appendix Method - Complete Set of Methods

Free Engineering Spreadsheets: Loads - Simplified Part 23 Aircraft Loads, Part 23 Appendix Method - Complete Set of Methods. 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-515

 


5 March 2017 Spreadsheet updated to include all control surface, tab and flap loads. Spreadsheet renumbered to AA-SM-515-000 to allow for individual break-out sheets

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AA-SM-515-000 Loads - Simplified Part 23 Aircraft Loads - Complete.xlsxDownload 
AA-SM-515 Loads - Simplified Part 23 Aircraft Loads.xlsxDownload 

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AA-SM-515-000

  • Version
  • 2281 Downloads
  • 634.59 KB File Size
  • 2 File Count
  • March 13, 2016 Create Date
  • March 13, 2016 Last Updated
Scroll for Details

AA-SM-515-000 Loads - Simplified Part 23 Aircraft Loads, Part 23 Appendix Method - Complete Set of Methods

Free Engineering Spreadsheets: Loads - Simplified Part 23 Aircraft Loads, Part 23 Appendix Method - Complete Set of Methods. 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-515

 


5 March 2017 Spreadsheet updated to include all control surface, tab and flap loads. Spreadsheet renumbered to AA-SM-515-000 to allow for individual break-out sheets

FileAction
AA-SM-515-000 Loads - Simplified Part 23 Aircraft Loads - Complete.xlsxDownload 
AA-SM-515 Loads - Simplified Part 23 Aircraft Loads.xlsxDownload 
17,005 Documents in our Technical Library
2589846 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 ...