Explore: Boundary Layer Thickness

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Source: The Open Library

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1High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation

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“High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation” Metadata:

  • Title: ➤  High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
  • Author:
  • Language: English
  • Number of Pages: Median: 51
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - [Cleveland, Ohio]

“High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1999
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

Online Access

Downloads Are Not Available:

The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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    2Analysis of gas turbine rotor blade tip and shroud heat transfer

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    “Analysis of gas turbine rotor blade tip and shroud heat transfer” Metadata:

    • Title: ➤  Analysis of gas turbine rotor blade tip and shroud heat transfer
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Washington, DC - Springfield, Va

    “Analysis of gas turbine rotor blade tip and shroud heat transfer” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1996
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Marketplaces

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    3Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer

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    “Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer” Metadata:

    • Title: ➤  Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: Hampton, Va - [Springfield, Va

    “Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1997
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Access

    Downloads Are Not Available:

    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

    Online Borrowing:

      Online Marketplaces

      Find Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer at online marketplaces:


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