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+AVL is a program for the aerodynamic and flight-dynamic analysis of
+rigid aircraft of arbitrary configuration. It employs an extended
+vortex lattice model for the lifting surfaces, together with a
+slender-body model for fuselages and nacelles. General nonlinear flight
+states can be specified. The flight dynamic analysis combines a full
+linearization of the aerodynamic model about any flight state, together
+with specified mass properties.