http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
Noise computation of a shock-containing supersonic axisymmetric jet by the CE/SE method
Noise computation of a shock-containing supersonic axisymmetric jet by the conservation element solution element method
1 online resource (16 pages) : illustrations.
"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
Includes bibliographical references (pages 8-9).
Sponsored by the National Aeronautics and Space Administration WU-522-81-11-00 E-12029