Sandberg, R.D. and Fasel, H.F. (2004) Application of a new flow simulation methodology for supersonic axisymmetric wakes. AIAA 42nd Aerospace Sciences Meeting & Exhibit, Reno, United States. 05 - 08 Jan 2004.
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Published date: January 2004
Venue - Dates:
AIAA 42nd Aerospace Sciences Meeting & Exhibit, Reno, United States, 2004-01-05 - 2004-01-08
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Organisations:
Aerodynamics & Flight Mechanics
Identifiers
Local EPrints ID: 185821
URI: http://eprints.soton.ac.uk/id/eprint/185821
PURE UUID: 0a2a18ab-0ea7-496e-9826-4e70c909b716
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Date deposited: 03 Jun 2011 13:36
Last modified: 08 Jan 2022 11:39
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Contributors
Author:
R.D. Sandberg
Author:
H.F. Fasel
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