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NASA NTRS · 19730022194

Finite element analysis and computer graphics visualization of flow around pitching and plunging airfoils

Abstract

A general computational method for analyzing unsteady flow around pitching and plunging airfoils was developed. The finite element method was applied in developing an efficient numerical procedure for the solution of equations describing the flow around airfoils. The numerical results were employed in conjunction with computer graphics techniques to produce visualization of the flow. The investigation involved mathematical model studies of flow in two phases: (1) analysis of a potential flow formulation and (2) analysis of an incompressible, unsteady, viscous flow from Navier-Stokes equations.

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BibTeXRIS

Bratanow, T., Ecer, A.. 1973-09-01. Finite element analysis and computer graphics visualization of flow around pitching and plunging airfoils. https://ntrs.nasa.gov/citations/19730022194

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