NASA NTRS · 19890003519
Aerothermal modeling program, phase 2
Abstract
The main objective of the NASA sponsored Aerothermal Modeling Program, Phase 2--Element A, is to develop an improved numerical scheme for predicting combustor flow fields. This effort consists of the following three technical tasks. Task 1 involves the selection and evaluation of various candidate numerical techniques. Task 2 involves an in-depth evaluation of the selected numerical schemes. Task 3 involves the convection-diffusion scheme and the direct solver that will be incorporated in the NASA 3-D elliptic code (COM3S).
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Karki, K. C., Mongia, H. C., Patankar, Suhas V., Runchal, A. K.. 1986-10-01. Aerothermal modeling program, phase 2. https://ntrs.nasa.gov/citations/19890003519
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