English
VSAERO is a computer program used to predict the nonlinear aerodynamic characteristics of arbitrary three-dimensional configurations in subsonic flow. Nonlinear effects of vortex separation and vortex surface interaction are treated in an iterative wake-shape calculation procedure, while the effects of viscosity are treated in an iterative loop coupling potential-flow and integral boundary-layer calculations. The program employs a surface singularity panel method using quadrilateral panels on which doublet and source singularities are distributed in a piecewise constant form. This user's manual provides a brief overview of the mathematical model, instructions for configuration modeling and a description of the input and output data. A listing of a sample case is included.
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Ebook · NASA Technical Reports Server (NTRS) 19850006493: PROGRAM VSAERO: A computer program for calculating the non-linear aerodynamic characteristics of arbitrary configurations: User's manual · NASA Technical Reports Server (NTRS) · Internet Archive
NASA Technical Reports Server (NTRS) · AERODYNAMIC CHARACTERISTICS · COMPUTER PROGRAMS · NONLINEARITY · SUBSONIC FLOW · USER MANUALS (COMPUTER PROGRAMS) · BOUNDARY LAYERS · ITERATIVE SOLUTION · MATHEMATICAL MODELS · PANEL METHOD (FLUID DYNAMICS)