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A Three-Dimensional Solution of Flows over Wings with Leading-Edge Vortex Separation. Part 2: Program Description Document

Roger G. Coleman, Forrester T. Johnson, P. Lu

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Abstract

A computer program has been developed for the solution of the subsonic, three-dimensional flow over wings with leading-edge vortex separation.The documentation is divided into two volumes, Part I and Part II. This volume is Part II of the documentation containing the description of the computer program. It consists of three sections presenting the Program Logic, the Description of Subroutines, and the Program Listing.

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A computer program has been developed for the solution of the subsonic, three-dimensional flow over wings with leading-edge vortex separation.The documentation is divided into two volumes, Part I and Part II. This volume is Part II of the documentation containing the description of the computer program. It consists of three sections presenting the Program Logic, the Description of Subroutines, and the Program Listing.

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Available abstract

A computer program has been developed for the solution of the subsonic, three-dimensional flow over wings with leading-edge vortex separation.The documentation is divided into two volumes, Part I and Part II. This volume is Part II of the documentation containing the description of the computer program. It consists of three sections presenting the Program Logic, the Description of Subroutines, and the Program Listing.

Key concepts: Vortex, Separation (statistics), Enhanced Data Rates for GSM Evolution, Leading edge, Geometry, Mechanics, Computer science, Classical mechanics

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