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Source: The Open Library

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1Effect of in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models

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“Effect of in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models” Metadata:

  • Title: ➤  Effect of in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models
  • Author:
  • Language: English
  • Number of Pages: Median: 50
  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - Washington, D.C

“Effect of in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models” 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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2Thrust-reverser flow investigation on a twin-engine transport

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“Thrust-reverser flow investigation on a twin-engine transport” Metadata:

  • Title: ➤  Thrust-reverser flow investigation on a twin-engine transport
  • Author:
  • Language: English
  • Number of Pages: Median: 153
  • Publisher: ➤  Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Division - For sale by the National Technical Information Service]
  • Publish Date:
  • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, D.C.]

“Thrust-reverser flow investigation on a twin-engine transport” 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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    3Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds

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    “Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds” Metadata:

    • Title: ➤  Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds
    • Author:
    • Language: English
    • Number of Pages: Median: 88
    • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - Washington, D.C

    “Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1983
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Marketplaces

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    4Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20

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    “Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20” Metadata:

    • Title: ➤  Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20
    • Author:
    • Language: English
    • Number of Pages: Median: 188
    • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration
    • Publish Date:
    • Publish Location: Washington - Springfield, Va

    “Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20” 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

    Online Marketplaces

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    5Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers

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    “Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers” Metadata:

    • Title: ➤  Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers
    • Author:
    • Language: English
    • Number of Pages: Median: 168
    • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
    • Publish Date:
    • Publish Location: ➤  Washington, D.C - [Springfield, Va

    “Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1982
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    6Silovye ustanovki s povorotom vektora ti͡a︡gi v polete

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    “Silovye ustanovki s povorotom vektora ti͡a︡gi v polete” Metadata:

    • Title: ➤  Silovye ustanovki s povorotom vektora ti͡a︡gi v polete
    • Author: ➤  
    • Language: rus
    • Number of Pages: Median: 196
    • Publisher: "Mashinostroenie"
    • Publish Date:
    • Publish Location: Moskva

    “Silovye ustanovki s povorotom vektora ti͡a︡gi v polete” 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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    7Reversivnye ustroĭstva silovykh ustanovok s vozdushno-reaktivnymi dvigateli͡ami

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    “Reversivnye ustroĭstva silovykh ustanovok s vozdushno-reaktivnymi dvigateli͡ami” Metadata:

    • Title: ➤  Reversivnye ustroĭstva silovykh ustanovok s vozdushno-reaktivnymi dvigateli͡ami
    • Author: ➤  
    • Language: rus
    • Number of Pages: Median: 208
    • Publisher: ➤  Vses. in-t nauch. i tekhn. informat͡sii
    • Publish Date:
    • Publish Location: Moskva

    “Reversivnye ustroĭstva silovykh ustanovok s vozdushno-reaktivnymi dvigateli͡ami” Subjects and Themes:

    Edition Identifiers:

    • The Open Library ID: OL3855401M
    • Online Computer Library Center (OCLC) ID: 13497139
    • Library of Congress Control Number (LCCN): 81174609

    Access and General Info:

    • First Year Published: 1978
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Marketplaces

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    8Static internal performance including thrust vectoring and reversing of tow-dimensional convergent-divergent nozzles

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    “Static internal performance including thrust vectoring and reversing of tow-dimensional convergent-divergent nozzles” Metadata:

    • Title: ➤  Static internal performance including thrust vectoring and reversing of tow-dimensional convergent-divergent nozzles
    • Author:
    • Language: English
    • Number of Pages: Median: 108
    • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
    • Publish Date:
    • Publish Location: ➤  Washington, D.C - [Springfield, Va

    “Static internal performance including thrust vectoring and reversing of tow-dimensional convergent-divergent nozzles” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1984
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Marketplaces

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    9Internal pressure distributions for a two-dimensional thrust-reversing nozzle operating at a free-stream mach number of zero

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    “Internal pressure distributions for a two-dimensional thrust-reversing nozzle operating at a free-stream mach number of zero” Metadata:

    • Title: ➤  Internal pressure distributions for a two-dimensional thrust-reversing nozzle operating at a free-stream mach number of zero
    • Author:
    • Language: English
    • Number of Pages: Median: 42
    • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
    • Publish Date:
    • Publish Location: ➤  Washington, D.C - [Springfield, Va

    “Internal pressure distributions for a two-dimensional thrust-reversing nozzle operating at a free-stream mach number of zero” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1983
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Marketplaces

    Find Internal pressure distributions for a two-dimensional thrust-reversing nozzle operating at a free-stream mach number of zero at online marketplaces:


    10Static internal performance characteristics of two thrust-reverser concepts for axisymmetric nozzles

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    “Static internal performance characteristics of two thrust-reverser concepts for axisymmetric nozzles” Metadata:

    • Title: ➤  Static internal performance characteristics of two thrust-reverser concepts for axisymmetric nozzles
    • Author:
    • Language: English
    • Number of Pages: Median: 21
    • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
    • Publish Date:
    • Publish Location: ➤  Washington, D.C - [Springfield, Va. : For sale by the National Technical Information Service]

    “Static internal performance characteristics of two thrust-reverser concepts for axisymmetric nozzles” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1982
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Marketplaces

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    11Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers

    By

    “Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers” Metadata:

    • Title: ➤  Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers
    • Author:
    • Language: English
    • Number of Pages: Median: 168
    • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
    • Publish Date:
    • Publish Location: ➤  Washington, D.C - [Springfield, Va

    “Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1982
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Marketplaces

    Find Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers at online marketplaces:


    12Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability

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    “Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability” Metadata:

    • Title: ➤  Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
    • Publish Date:
    • Publish Location: [Washington, D.C.]

    “Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1989
    • 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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      13Effect of varying internal geometry on the static performance of rectangular thrust-reverser ports

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      “Effect of varying internal geometry on the static performance of rectangular thrust-reverser ports” Metadata:

      • Title: ➤  Effect of varying internal geometry on the static performance of rectangular thrust-reverser ports
      • Author:
      • Language: English
      • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
      • Publish Date:
      • Publish Location: ➤  [Springfield, Va - [Washington, DC]

      “Effect of varying internal geometry on the static performance of rectangular thrust-reverser ports” 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

      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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        14Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap

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        “Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap” Metadata:

        • Title: ➤  Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
        • Publish Date:
        • Publish Location: ➤  [Washington, D.C.] - Springfield, Va

        “Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap” 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.

        Online Borrowing:

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          15Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser

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          “Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser” Metadata:

          • Title: ➤  Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
          • Publish Date:
          • Publish Location: ➤  [Springfield, Va - [Washington, DC]

          “Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser” 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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            16Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser

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            “Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser” Metadata:

            • Title: ➤  Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Division - For sale by the National Technical Information Service]
            • Publish Date:
            • Publish Location: ➤  [Springfield, Va - [Washington, DC]

            “Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser” 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.

            Online Borrowing:

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              17Systems for deflection of the jet streams of turbo-jet engines

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              “Systems for deflection of the jet streams of turbo-jet engines” Metadata:

              • Title: ➤  Systems for deflection of the jet streams of turbo-jet engines
              • Author: ➤  
              • Language: English
              • Number of Pages: Median: 202
              • Publisher: ➤  for sale by the Clearinghouse for Federal Scientific and Technical Information - National Aeronautics and Space Administration - National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.
              • Publish Date:
              • Publish Location: [Washington]

              “Systems for deflection of the jet streams of turbo-jet engines” Subjects and Themes:

              Edition Identifiers:

              • The Open Library ID: OL4854748M
              • Online Computer Library Center (OCLC) ID: 87048
              • Library of Congress Control Number (LCCN): 75606647

              Access and General Info:

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

              Online Marketplaces

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