Vortex-Lattice UtilizationThe many novel, innovative, and unique implementations and applications of the vortex-lattice method to aerodynamic design and analysis which have been performed by Industry, Government, and Universities were presented. Although this analytical tool is not new, it continues to be utilized and refined in the aeronautical community.
IDRelationTitle19760021085WorkA quadrilateral vortex method applied to configurations with high circulation19760021098WorkSample wings for study19760021097WorkUnsteady flow past wings having sharp-edge separation19760021081WorkMinimum trim drag design for interfering lifting surfaces using vortex-lattice methodology19760021076WorkHistorical evolution of vortex-lattice methods19760021082WorkApplications of vortex lattice theory to preliminary aerodynamic design19760021077WorkSubsonic finite elements for wing body combinations19760021086WorkUpper-surface-blowing jet wing interaction19760021084WorkReport on the status of a slotted wind tunnel wall representation using the vortex-lattice technique19760021079WorkNumerical method to calculate the induced drag or optimum loading for arbitrary non-planar aircraft19760021078WorkExtended applications of the vortex lattice method19760021095WorkA subvortex technique for the close approach to a discretized vortex sheet19760021080WorkOptimization and design of three-dimensional aerodynamic configurations of arbitrary shape by a vortex lattice method19760021096WorkSome applications of the quasi vortex-lattice method in steady and unsteady aerodynamics19760021088WorkSome recent applications of the suction analogy to asymmetric flow situations19760021092WorkArrangement of vortex lattices19760021093WorkLattice arrangements for rapid convergence19760021091WorkNew convergence criteria for the vortex-lattice models of the leading-edge separation19760021087WorkCalculation of the longitudinal aerodynamic characteristics of wing-flap configurations with externally blown flaps19760021089WorkApplication of the vortex-lattice technique to the analysis of thin wings with vortex separation and thick multi-element wings19760021083WorkUtilization of the AEDC three-dimensional potential flow computer program19760021090WorkComparison of vortex lattice predicted forces with wind tunnel experiments for the F-4E(CCV) airplane with a closely coupled canard19760021094WorkOptimum lattice arrangement developed from a rigorous analytical basis