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What is Aerodynamic Influence Coefficient Matrix about?

The purpose of this appendix is to derive expressions for computing the Aerodynamic influence coefficient matrix (or [AI matrix) for nonplanar wing-body-tail configurations. An aerodynamic influence coefficient aij (i.e. an element of the A matrix) is defined as the load in lbs. (Newtons) induced on panel i as a result of a unit angle of attack (rad) on panel j. Simulation of wing-body interference is not attempted.

Author

Mongoose82

Language

EN