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Source: The Open Library

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1Beitrag zur Untersuchung rotationssymmetrischer Tandemgitter für Überschallströmung

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Book's cover

“Beitrag zur Untersuchung rotationssymmetrischer Tandemgitter für Überschallströmung” Metadata:

  • Title: ➤  Beitrag zur Untersuchung rotationssymmetrischer Tandemgitter für Überschallströmung
  • Author:
  • Language: ger
  • Number of Pages: Median: 95
  • Publisher: ➤  VS Verlag für Sozialwissenschaften - Westdeutscher Verlag
  • Publish Date:
  • Publish Location: Köln

“Beitrag zur Untersuchung rotationssymmetrischer Tandemgitter für Überschallströmung” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1970
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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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 fully stalled compressor

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    “Analysis of fully stalled compressor” Metadata:

    • Title: ➤  Analysis of fully stalled compressor
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
    • Publish Date:
    • Publish Location: [Cleveland, Ohio

    “Analysis of fully stalled compressor” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1986
    • 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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      3Mass balancing of hollow fan blades

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      “Mass balancing of hollow fan blades” Metadata:

      • Title: ➤  Mass balancing of hollow fan blades
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
      • Publish Date:
      • Publish Location: [Cleveland, Ohio

      “Mass balancing of hollow fan blades” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1986
      • 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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        4Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations

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        “Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations” Metadata:

        • Title: ➤  Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations
        • Author:
        • Language: English
        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
        • Publish Date:
        • Publish Location: ➤  Springfield, Va - [Washington, DC

        “Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1998
        • 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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          5Supersonic propulsion simulation by incorporating component models in the Large Pertubation Inlet (LAPIN) computer code

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          “Supersonic propulsion simulation by incorporating component models in the Large Pertubation Inlet (LAPIN) computer code” Metadata:

          • Title: ➤  Supersonic propulsion simulation by incorporating component models in the Large Pertubation Inlet (LAPIN) computer code
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration
          • Publish Date:
          • Publish Location: [Washington, DC]

          “Supersonic propulsion simulation by incorporating component models in the Large Pertubation Inlet (LAPIN) computer code” 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

          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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            6Interaction entre une onde de choc oblique et une grille d'aubes fixes parcourues par un écoulement subsonique

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            “Interaction entre une onde de choc oblique et une grille d'aubes fixes parcourues par un écoulement subsonique” Metadata:

            • Title: ➤  Interaction entre une onde de choc oblique et une grille d'aubes fixes parcourues par un écoulement subsonique
            • Author:
            • Language: fre
            • Number of Pages: Median: 181
            • Publisher: Juris-Verlag
            • Publish Date:
            • Publish Location: Zürich

            “Interaction entre une onde de choc oblique et une grille d'aubes fixes parcourues par un écoulement subsonique” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1977
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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