AA-SM-504 Loads – Modification to Wing Lift Gradient for Compressibility
Sample Engineering Spreadsheets Provided by Abbott Aerospace Inc
This spreadsheet uses the XL-Viking Plugin to display equations. The Spreadsheet will calculate correctly without the plugin and can be used ‘as is’ but none of the math will be visible. To find out more about XL-Viking click here
Spreadsheet to calculate the increase in airfoil lift gradient at speed below mach 1.