Date of Award
12-1991
Document Type
Thesis
Degree Name
Master of Science
Department
Department of Aeronautics and Astronautics
First Advisor
John H. Doty, PhD
Abstract
This research investigated the effects of adding a second-order flux- difference-splitting (FDS) correction term to an existing computer code that is based on a first-order FDS algorithm. It was determined that the second-order algorithm did improve the accuracy of the code for a source flow analysis, but second-order behavior could not be confirmed by the error convergence patterns. It was also discovered that, when tested across an oblique shock wave, the second-order correction terms had minimal influence on the accuracy and shock capturing ability of the first-order accurate FDS method.
AFIT Designator
AFIT-GAE-ENY-91D-13
DTIC Accession Number
ADA244047
Recommended Citation
Allen, Danny P., "Investigation of a Flux-Difference-Splitting Numerical Method in Supersonic Nozzles" (1991). Theses and Dissertations. 7464.
https://scholar.afit.edu/etd/7464
Comments
The author's Vita page is omitted.