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Source: The Open Library

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1Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment

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“Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment” Metadata:

  • Title: ➤  Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment
  • Author:
  • Language: English
  • Number of Pages: Median: 27
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - Langley Research Center
  • Publish Date:
  • Publish Location: Hampton, Va - [Springfield, Va

“Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1994
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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    2An approach to the design of airfoils with high lift to drag ratios

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    “An approach to the design of airfoils with high lift to drag ratios” Metadata:

    • Title: ➤  An approach to the design of airfoils with high lift to drag ratios
    • Author:
    • Number of Pages: Median: 59
    • Publisher: ➤  Institute for Aerospace Studies - Dept. of Aerospace Science and Engineering
    • Publish Date:
    • Publish Location: [Downsview, Ont.]

    “An approach to the design of airfoils with high lift to drag ratios” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1981
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    3A new iterative matrix solution procedure for three-dimensional panel methods

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    “A new iterative matrix solution procedure for three-dimensional panel methods” Metadata:

    • Title: ➤  A new iterative matrix solution procedure for three-dimensional panel methods
    • Author:
    • Publisher: AIAA
    • Publish Date:
    • Publish Location: New York

    “A new iterative matrix solution procedure for three-dimensional panel methods” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1985
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    4Development and analysis of panel methods for propellers in unsteady flow

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    “Development and analysis of panel methods for propellers in unsteady flow” Metadata:

    • Title: ➤  Development and analysis of panel methods for propellers in unsteady flow
    • Author:
    • Number of Pages: Median: 156
    • Publisher: ➤  Massachusetts Institute of Technology
    • Publish Date:
    • Publish Location: [Cambridge, Mass.]

    “Development and analysis of panel methods for propellers in unsteady flow” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1990
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    5On the use of "panel methods" for predicting subsonic flow about aerofoils and aircraft configurations

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    “On the use of "panel methods" for predicting subsonic flow about aerofoils and aircraft configurations” Metadata:

    • Title: ➤  On the use of "panel methods" for predicting subsonic flow about aerofoils and aircraft configurations
    • Author:
    • Number of Pages: Median: 15
    • Publisher: National Aerospace Laboratory
    • Publish Date:
    • Publish Location: [Amsterdam, the Netherlands]

    “On the use of "panel methods" for predicting subsonic flow about aerofoils and aircraft configurations” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1971
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    6An investigation into the interface between three closely spaced axi-symmetric bodies at subsonic speed

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    “An investigation into the interface between three closely spaced axi-symmetric bodies at subsonic speed” Metadata:

    • Title: ➤  An investigation into the interface between three closely spaced axi-symmetric bodies at subsonic speed
    • Author:
    • Number of Pages: Median: 112
    • Publisher: ➤  Cranfield Institute of Technology, College of Aeronautics
    • Publish Date:
    • Publish Location: Cranfield, Bedford, England

    “An investigation into the interface between three closely spaced axi-symmetric bodies at subsonic speed” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1991
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    7CAR 88

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    “CAR 88” Metadata:

    • Title: CAR 88
    • Author:
    • Number of Pages: Median: 72
    • Publisher: National Aerospace Laboratory
    • Publish Date:
    • Publish Location: Amsterdam

    “CAR 88” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1988
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    8Development of an advanced panel method for complex configurations in subsonic compressible flow; application to the computation of the potential flow through ducts

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    “Development of an advanced panel method for complex configurations in subsonic compressible flow; application to the computation of the potential flow through ducts” Metadata:

    • Title: ➤  Development of an advanced panel method for complex configurations in subsonic compressible flow; application to the computation of the potential flow through ducts
    • Author:
    • Number of Pages: Median: 45
    • Publisher: National Aerospace Laboratory
    • Publish Date:
    • Publish Location: Amsterdam, Netherlands

    “Development of an advanced panel method for complex configurations in subsonic compressible flow; application to the computation of the potential flow through ducts” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1987
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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