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Source: The Open Library

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1Pizza

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Book's cover

“Pizza” Metadata:

  • Title: Pizza
  • Author:
  • Language: ➤  Spanish; Castilian - español, castellano
  • Number of Pages: Median: 16
  • Publisher: Scholastic Paperbacks
  • Publish Date:

“Pizza” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 2000
  • Is Full Text Available: Yes
  • Is The Book Public: No
  • Access Status: Borrowable

Online Access

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2A theory for the roll-ratchet phenomenon in high performance aircraft

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“A theory for the roll-ratchet phenomenon in high performance aircraft” Metadata:

  • Title: ➤  A theory for the roll-ratchet phenomenon in high performance aircraft
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
  • Publish Date:
  • Publish Location: ➤  Springfield, Va - [Washington, DC

“A theory for the roll-ratchet phenomenon in high performance aircraft” 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.

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    3Scooby-Doo! Cheese Mystery

    Sight Words Book 4

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    Book's cover

    “Scooby-Doo! Cheese Mystery” Metadata:

    • Title: Scooby-Doo! Cheese Mystery
    • Author:
    • Language: English
    • Number of Pages: Median: 16
    • Publisher: Scholastic, Inc
    • Publish Date:
    • Publish Location: New York, USA

    “Scooby-Doo! Cheese Mystery” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 2011
    • 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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      4Roll-yaw control at high angle of attack by forebody tangential blowing

      “Roll-yaw control at high angle of attack by forebody tangential blowing” Metadata:

      • Title: ➤  Roll-yaw control at high angle of attack by forebody tangential blowing
      • Language: English
      • Publisher: ➤  Joint Institute for Aeronautics and Acoustics - National Technical Information Service, distributor - National Aeronautics and Space Administration
      • Publish Date:
      • Publish Location: ➤  [Stanford, Calif.?] - Springfield, Va - [Washington, DC

      “Roll-yaw control at high angle of attack by forebody tangential blowing” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1995
      • 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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        5Goma de borrar, aventuras y desventuras del chico perfecto

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        Book's cover

        “Goma de borrar, aventuras y desventuras del chico perfecto” Metadata:

        • Title: ➤  Goma de borrar, aventuras y desventuras del chico perfecto
        • Author:
        • Language: ➤  Spanish; Castilian - español, castellano
        • Number of Pages: Median: 415
        • Publisher: Taranna Edicions, SCP
        • Publish Date:
        • Publish Location: Barcelona, Spain

        “Goma de borrar, aventuras y desventuras del chico perfecto” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 2010
        • 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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          6Scuffing characteristics of high-load rolling/sliding contacts operating in liquid oxygen

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          “Scuffing characteristics of high-load rolling/sliding contacts operating in liquid oxygen” Metadata:

          • Title: ➤  Scuffing characteristics of high-load rolling/sliding contacts operating in liquid oxygen
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  Springfield, Va - [Washington, DC

          “Scuffing characteristics of high-load rolling/sliding contacts operating in liquid oxygen” 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 Access

          Downloads Are Not Available:

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            7Active load control during rolling maneuvers

            By

            “Active load control during rolling maneuvers” Metadata:

            • Title: ➤  Active load control during rolling maneuvers
            • Author:
            • Language: English
            • Publisher: ➤  National Technical Information Service [distributor - National Aeronautics and Space Administration, Langley Research Center
            • Publish Date:
            • Publish Location: Springfield, VA - Hampton, Va

            “Active load control during rolling maneuvers” 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

            Online Access

            Downloads Are Not Available:

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              8A parametric study of accelerations of an airplane due to a wake vortex system

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              “A parametric study of accelerations of an airplane due to a wake vortex system” Metadata:

              • Title: ➤  A parametric study of accelerations of an airplane due to a wake vortex system
              • 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

              “A parametric study of accelerations of an airplane due to a wake vortex system” 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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                9Design considerations of manipulator and feel system characteristics in roll tracking

                By

                “Design considerations of manipulator and feel system characteristics in roll tracking” Metadata:

                • Title: ➤  Design considerations of manipulator and feel system characteristics in roll tracking
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Division
                • Publish Date:
                • Publish Location: [Washington, D.C.]

                “Design considerations of manipulator and feel system characteristics in roll tracking” 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

                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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                  10An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities

                  By

                  “An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities” Metadata:

                  • Title: ➤  An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
                  • Publish Date:
                  • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                  “An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1995
                  • 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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                    11Experiments in aircraft roll-yaw control using forebody tangential blowing

                    By

                    “Experiments in aircraft roll-yaw control using forebody tangential blowing” Metadata:

                    • Title: ➤  Experiments in aircraft roll-yaw control using forebody tangential blowing
                    • Author:
                    • Language: English
                    • Publisher: ➤  Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor - Joint Institute for Aeronautics and Acoustics, Stanford University
                    • Publish Date:
                    • Publish Location: ➤  [Stanford, Calif.] - [Springfield, Va

                    “Experiments in aircraft roll-yaw control using forebody tangential blowing” 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.

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                      12Determination of shuttle orbiter center of gravity from flight measurements

                      By

                      “Determination of shuttle orbiter center of gravity from flight measurements” Metadata:

                      • Title: ➤  Determination of shuttle orbiter center of gravity from flight measurements
                      • Author:
                      • Language: English
                      • Publisher: NASA Langley Research Center
                      • Publish Date:
                      • Publish Location: Hampton, Va

                      “Determination of shuttle orbiter center of gravity from flight measurements” 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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                        13Two blowing concepts for roll and lateral control of aircraft

                        By

                        “Two blowing concepts for roll and lateral control of aircraft” Metadata:

                        • Title: ➤  Two blowing concepts for roll and lateral control of aircraft
                        • Author:
                        • Number of Pages: Median: 102
                        • Publisher: ➤  Dept. of Aeronautics and Astronautics, Stanford University
                        • Publish Date:
                        • Publish Location: Stanford, Calif

                        “Two blowing concepts for roll and lateral control of aircraft” 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

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                        14Annual Report

                        By

                        Book's cover

                        “Annual Report” Metadata:

                        • Title: Annual Report
                        • Authors: ➤  
                        • Number of Pages: Median: 99
                        • Publish Date:

                        “Annual Report” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1866
                        • Is Full Text Available: Yes
                        • Is The Book Public: Yes
                        • Access Status: Public

                        Online Access

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