Abstract
This report describes recent progress in the development and application of 3D Cartesian grid generation and Euler flow solution techniques. Improvements to flow field grid generation algorithms, geometry representations, and geometry refinement criteria are presented, including details of a procedure for correctly identifying and resolving extremely thin surface features. An initial implementation of automatic flow field refinement is also presented. Results for several 3D multi-component configurations are provided and discussed.
| Original language | English (US) |
|---|---|
| Title of host publication | 33rd Aerospace Sciences Meeting and Exhibit |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| ISBN (Print) | 9780000000002 |
| State | Published - 1995 |
| Event | 33rd Aerospace Sciences Meeting and Exhibit, 1995 - Reno, United States Duration: Jan 9 1995 → Jan 12 1995 |
Other
| Other | 33rd Aerospace Sciences Meeting and Exhibit, 1995 |
|---|---|
| Country | United States |
| City | Reno |
| Period | 1/9/95 → 1/12/95 |
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ASJC Scopus subject areas
- Space and Planetary Science
- Aerospace Engineering
Cite this
3D applications of a Cartesian grid Euler method. / Melton, John E.; Berger, Marsha; Aftosmis, Michael J.; Wong, Michael D.
33rd Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA, 1995. AlAA 95-0853.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - 3D applications of a Cartesian grid Euler method
AU - Melton, John E.
AU - Berger, Marsha
AU - Aftosmis, Michael J.
AU - Wong, Michael D.
PY - 1995
Y1 - 1995
N2 - This report describes recent progress in the development and application of 3D Cartesian grid generation and Euler flow solution techniques. Improvements to flow field grid generation algorithms, geometry representations, and geometry refinement criteria are presented, including details of a procedure for correctly identifying and resolving extremely thin surface features. An initial implementation of automatic flow field refinement is also presented. Results for several 3D multi-component configurations are provided and discussed.
AB - This report describes recent progress in the development and application of 3D Cartesian grid generation and Euler flow solution techniques. Improvements to flow field grid generation algorithms, geometry representations, and geometry refinement criteria are presented, including details of a procedure for correctly identifying and resolving extremely thin surface features. An initial implementation of automatic flow field refinement is also presented. Results for several 3D multi-component configurations are provided and discussed.
UR - http://www.scopus.com/inward/record.url?scp=2942730074&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=2942730074&partnerID=8YFLogxK
M3 - Conference contribution
SN - 9780000000002
BT - 33rd Aerospace Sciences Meeting and Exhibit
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
ER -