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Effect of wake structure on blade-vortex interaction phenomena: Acoustic prediction and validation.

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Bibliographic Details
Title: Effect of wake structure on blade-vortex interaction phenomena: Acoustic prediction and validation.
Authors: Gallman, Judith M., Schultz, Klaus-J., Spiegel, Pierre, Burley, Casey L.
Source: Journal of Aircraft. Mar/Apr98, Vol. 35 Issue 2, p267. 7p. 1 Diagram, 2 Charts, 73 Graphs.
Subjects: Vortex motion, Mathematical models
Abstract: Discusses the improvements made to the blade-vortex interaction (BVI) modeling after the evaluation of the test data. How to correctly predict the aerodynamic and acoustic pressure for a helicopter operation in powered descent flight; Test and model description; Results and discussion.
Database: Engineering Source
FullText Text:
  Availability: 0
Header DbId: egs
DbLabel: Engineering Source
An: 454216
AccessLevel: 6
PubType: Academic Journal
PubTypeId: academicJournal
PreciseRelevancyScore: 0
IllustrationInfo
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  Data: Effect of wake structure on blade-vortex interaction phenomena: Acoustic prediction and validation.
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  Data: <searchLink fieldCode="AR" term="%22Gallman%2C+Judith+M%2E%22">Gallman, Judith M.</searchLink><br /><searchLink fieldCode="AR" term="%22Schultz%2C+Klaus-J%2E%22">Schultz, Klaus-J.</searchLink><br /><searchLink fieldCode="AR" term="%22Spiegel%2C+Pierre%22">Spiegel, Pierre</searchLink><br /><searchLink fieldCode="AR" term="%22Burley%2C+Casey+L%2E%22">Burley, Casey L.</searchLink>
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  Data: <searchLink fieldCode="JN" term="%22Journal+of+Aircraft%22">Journal of Aircraft</searchLink>. Mar/Apr98, Vol. 35 Issue 2, p267. 7p. 1 Diagram, 2 Charts, 73 Graphs.
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  Data: <searchLink fieldCode="DE" term="%22Vortex+motion%22">Vortex motion</searchLink><br /><searchLink fieldCode="DE" term="%22Mathematical+models%22">Mathematical models</searchLink>
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  Data: Discusses the improvements made to the blade-vortex interaction (BVI) modeling after the evaluation of the test data. How to correctly predict the aerodynamic and acoustic pressure for a helicopter operation in powered descent flight; Test and model description; Results and discussion.
PLink https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&db=egs&AN=454216
RecordInfo BibRecord:
  BibEntity:
    Identifiers:
      – Type: doi
        Value: 10.2514/2.2294
    Languages:
      – Code: eng
        Text: English
    PhysicalDescription:
      Pagination:
        PageCount: 7
        StartPage: 267
    Subjects:
      – SubjectFull: Vortex motion
        Type: general
      – SubjectFull: Mathematical models
        Type: general
    Titles:
      – TitleFull: Effect of wake structure on blade-vortex interaction phenomena: Acoustic prediction and validation.
        Type: main
  BibRelationships:
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      – PersonEntity:
          Name:
            NameFull: Gallman, Judith M.
      – PersonEntity:
          Name:
            NameFull: Schultz, Klaus-J.
      – PersonEntity:
          Name:
            NameFull: Spiegel, Pierre
      – PersonEntity:
          Name:
            NameFull: Burley, Casey L.
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      – BibEntity:
          Dates:
            – D: 01
              M: 03
              Text: Mar/Apr98
              Type: published
              Y: 1998
          Identifiers:
            – Type: issn-print
              Value: 00218669
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            – Type: volume
              Value: 35
            – Type: issue
              Value: 2
          Titles:
            – TitleFull: Journal of Aircraft
              Type: main
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