Advanced aerodynamic research. Final technical report [electronic resource].

Published: Washington, D.C. : United States. Dept. of Defense, 1993.
Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy.
Physical Description: 55 pages : digital, PDF file
Additional Creators: Los Alamos National Laboratory, United States. Department of Defense, and United States. Department of Energy. Office of Scientific and Technical Information

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Summary

A two-dimensional inviscid flow-field code was developed to assess the magnitude and impact of local pressure variations on a curved planar surface. The code uses a unique formation of the governing conservation equations in curvilinear streamtube coordinates which provides automatic grid generation and step control which are transparent to the user. The code is designed for straightforward extension to mixing-coupled condensing flows. This report includes (1) descriptions of the physical model and computer code; (2) example flow-field predictions/comparisons for selected test cases, and (3) a plan for code implementation to address and evaluate the condensation phenomena.

Report Numbers

E 1.99:la-sub--95-29
la-sub--95-29

Subject(s)

Engineering

Other Subject(s)

Note

Published through SciTech Connect.
12/01/1993.
"la-sub--95-29"
"DE95007644"
""
Freeman, G.N.; Scriven, G.R.

Type of Report and Period Covered Note

Final; 12/01/1993 - 12/01/1993

Funding Information

W-7405-ENG-36

View MARC record | catkey: 14112631