The Resource The effect of nondeterministic parameters on shock-associated noise prediction modeling, Milo D. Dahl, Abbas Khavaran ; prepared for the 16th Aeroacoustics Conference cosponsored by the American Institute of Aeronautics and Astronautics and the Confederation of European Aerospace Societies, Stockholm, Sweden, June 7-9, 2010, (electronic resource)

The effect of nondeterministic parameters on shock-associated noise prediction modeling, Milo D. Dahl, Abbas Khavaran ; prepared for the 16th Aeroacoustics Conference cosponsored by the American Institute of Aeronautics and Astronautics and the Confederation of European Aerospace Societies, Stockholm, Sweden, June 7-9, 2010, (electronic resource)

Label
The effect of nondeterministic parameters on shock-associated noise prediction modeling
Title
The effect of nondeterministic parameters on shock-associated noise prediction modeling
Statement of responsibility
Milo D. Dahl, Abbas Khavaran ; prepared for the 16th Aeroacoustics Conference cosponsored by the American Institute of Aeronautics and Astronautics and the Confederation of European Aerospace Societies, Stockholm, Sweden, June 7-9, 2010
Creator
Contributor
Subject
Language
eng
Member of
Cataloging source
GPO
http://library.link/vocab/creatorDate
1956-
http://library.link/vocab/creatorName
Dahl, Milo D.
Government publication
federal national government publication
Illustrations
illustrations
Index
no index present
Literary form
non fiction
Nature of contents
  • dictionaries
  • bibliography
  • technical reports
http://library.link/vocab/relatedWorkOrContributorDate
  • 1953-
  • 2010
http://library.link/vocab/relatedWorkOrContributorName
  • Khavaran, Abbas
  • NASA Glenn Research Center
  • AIAA/CEAS Aeroacoustics Conference
Series statement
NASA/TM
Series volume
2010-216801
http://library.link/vocab/subjectName
  • Aerodynamic noise
  • Sensitivity analysis
  • Noise prediction
  • Supersonic jet flow
  • Mathematical models
  • Probability distribution functions
Label
The effect of nondeterministic parameters on shock-associated noise prediction modeling, Milo D. Dahl, Abbas Khavaran ; prepared for the 16th Aeroacoustics Conference cosponsored by the American Institute of Aeronautics and Astronautics and the Confederation of European Aerospace Societies, Stockholm, Sweden, June 7-9, 2010, (electronic resource)
Link
http://purl.fdlp.gov/GPO/gpo3600
Instantiates
Publication
Note
  • Title from title screen (viewed on Feb. 1, 2011)
  • "September 2010."
  • "AIAA-2010-3841."
Bibliography note
Includes bibliographical references (page 16)
Carrier category
online resource
Carrier category code
cr
Carrier MARC source
rdacarrier
Color
mixed
Content category
text
Content type code
txt
Content type MARC source
rdacontent
Control code
ocm699819497
Dimensions
unknown
Extent
1 online resource (24 pages)
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
c
Other physical details
illustrations.
Specific material designation
remote
System control number
(Sirsi) a1062436
Label
The effect of nondeterministic parameters on shock-associated noise prediction modeling, Milo D. Dahl, Abbas Khavaran ; prepared for the 16th Aeroacoustics Conference cosponsored by the American Institute of Aeronautics and Astronautics and the Confederation of European Aerospace Societies, Stockholm, Sweden, June 7-9, 2010, (electronic resource)
Link
http://purl.fdlp.gov/GPO/gpo3600
Publication
Note
  • Title from title screen (viewed on Feb. 1, 2011)
  • "September 2010."
  • "AIAA-2010-3841."
Bibliography note
Includes bibliographical references (page 16)
Carrier category
online resource
Carrier category code
cr
Carrier MARC source
rdacarrier
Color
mixed
Content category
text
Content type code
txt
Content type MARC source
rdacontent
Control code
ocm699819497
Dimensions
unknown
Extent
1 online resource (24 pages)
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
c
Other physical details
illustrations.
Specific material designation
remote
System control number
(Sirsi) a1062436

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