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NASA NTRS · 19780004420

Stability analysis for laminar flow control, part 1

Abstract

The basic equations for the stability analysis of flow over three dimensional swept wings are developed and numerical methods for their solution are surveyed. The equations for nonlinear stability analysis of three dimensional disturbances in compressible, three dimensional, nonparallel flows are given. Efficient and accurate numerical methods for the solution of the equations of stability theory were surveyed and analyzed.

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BibTeXRIS

Benney, D. J., Orszag, S. A.. 1977-10-01. Stability analysis for laminar flow control, part 1. https://ntrs.nasa.gov/citations/19780004420

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