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Turboduct prop advantageous for 0 to 0.06 Mach aircraft.

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Bibliographic Details
Title: Turboduct prop advantageous for 0 to 0.06 Mach aircraft.
Authors: Cahn, M. S.
Source: Sae Journal; March 1963, Vol. 71, p88-90, 3p
Database: Applied Science & Technology Source
FullText Text:
  Availability: 0
Header DbId: aci
DbLabel: Applied Science & Technology Source
An: 516091472
AccessLevel: 2
PubType: Periodical
PubTypeId: serialPeriodical
PreciseRelevancyScore: 0
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  Data: Turboduct prop advantageous for 0 to 0.06 Mach aircraft.
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  Data: <searchLink fieldCode="JN" term="%22Sae+Journal%22">Sae Journal</searchLink>; March 1963, Vol. 71, p88-90, 3p
PLink https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&db=aci&AN=516091472
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      – Code: eng
        Text: English
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      Pagination:
        PageCount: 3
        StartPage: 88
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      – TitleFull: Turboduct prop advantageous for 0 to 0.06 Mach aircraft.
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            NameFull: Cahn, M. S.
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            – D: 02
              M: 03
              Text: March 1963
              Type: published
              Y: 1963
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              Value: 0036066X
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              Value: 71
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            – TitleFull: Sae Journal
              Type: main
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