AA-SM-510 Loads – Incremental Wing Lift for Plain Flaps

October 23, 2014 12:13 pm

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

References:
Ref R&M Report 2622, The Aerodynamic Characteristics of Flaps, Young, 1953

Description:
Delta Cl for varying flap configurations.


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