TY - CONF
T1 - 3D applications of a Cartesian grid Euler method
AU - Melton, John E.
AU - Berger, Marsha J.
AU - Aftosmis, Michael J.
AU - Wong, Michael D.
N1 - Funding Information:
M. Berger was supponed in part by DOE grant DE-FG02-88ER25053, and by AFOSR grant F49620-94-1-0132. NASA’s Numerical Aerodynamic Simulation Facility provided much of the computer time used in this study. This suppon is gratefully acknowledged.
Publisher Copyright:
© 1995 by the American Institute of Aeronautics and Astronautics, Inc.
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.
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U2 - 10.2514/6.1995-853
DO - 10.2514/6.1995-853
M3 - Paper
AN - SCOPUS:2942730074
T2 - 33rd Aerospace Sciences Meeting and Exhibit, 1995
Y2 - 9 January 1995 through 12 January 1995
ER -