DOT-FAA-AR-95-29 Vol 1

DOT-FAA-AR-95-29 Vol 1This an attempt by the FAA to provide an overview of composite theory and application in the context of the regulations. DOT/FAA/AR/95-29 represents the state of the art in 1997. While the development of reliable and robust laminate failure modes has developed beyond what is presented here much of this is still current and all of it is useful.

 

 

 

 


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DOT-FAA-AR-95-29 Vol 1

DOT-FAA-AR-95-29 Vol 1This an attempt by the FAA to provide an overview of composite theory and application in the context of the regulations. DOT/FAA/AR/95-29 represents the state of the art in 1997. While the development of reliable and robust laminate failure modes has developed beyond what is presented here much of this is still current and all of it is useful.

 

 

 

 


AA SEZC Banner #6

To try our free Stress Analysis Engineering Spreadsheets click below

FREE ANALYSIS SPREADSHEETS 3

To try our Add-in for Microsoft Excel for Windows click below

XL-Viking 2

Comment On This Post

Your email address will not be published.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