Program Wing-Section :

Calculates Bending Stresses And Margin of Safety , For A Single Cell Rectangular Wing-Box

• All Units Are The Same Material , All Stringers Are Lipped
• Corner Stringers Are C-sections , All Other Stringers Are Z-sections
• Stringers Numbering Starts From The Upper Left Corner And Proceeds Clockwise
• First Version November 2008 , Updated October 2010

Solver Features :

• Checking Lip Efficiency For All Stringers
• Crippling / Failing / Inter-Rivet Buckling Stresses , For Each Stringer In The Section
• Center of Mass For Each Stringer , And Hence For The Complete Section , With The Moment Of Inertia About X-Axis
• Brief Summery For All Calculation Results