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Source: The Open Library

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1Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle

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“Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle” Metadata:

  • Title: ➤  Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle
  • Author:
  • Language: English
  • 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

“Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle” 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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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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    2A study of canard-wing interference using experimental pressure data at transonic speeds

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    “A study of canard-wing interference using experimental pressure data at transonic speeds” Metadata:

    • Title: ➤  A study of canard-wing interference using experimental pressure data at transonic speeds
    • Author:
    • Language: English
    • Number of Pages: Median: 68
    • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
    • Publish Date:
    • Publish Location: [Washington] - Springfield, Va

    “A study of canard-wing interference using experimental pressure data at transonic speeds” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1979
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    3Flight-determined stability and control derivatives for the F-111 TACT research aircraft

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    “Flight-determined stability and control derivatives for the F-111 TACT research aircraft” Metadata:

    • Title: ➤  Flight-determined stability and control derivatives for the F-111 TACT research aircraft
    • Author:
    • Language: English
    • Number of Pages: Median: 76
    • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Service
    • Publish Date:
    • Publish Location: Springfield, Va - [Washington]

    “Flight-determined stability and control derivatives for the F-111 TACT research aircraft” Subjects and Themes:

    Edition Identifiers:

    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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    4A grid-embedding transonic flow analysis computer program for wing/nacelle configurations

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    “A grid-embedding transonic flow analysis computer program for wing/nacelle configurations” Metadata:

    • Title: ➤  A grid-embedding transonic flow analysis computer program for wing/nacelle configurations
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center
    • Publish Date:
    • Publish Location: Moffett Field, Calif

    “A grid-embedding transonic flow analysis computer program for wing/nacelle configurations” 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 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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      5Fast euler solver for steady one-dimensional flows

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      “Fast euler solver for steady one-dimensional flows” Metadata:

      • Title: ➤  Fast euler solver for steady one-dimensional flows
      • Author:
      • Language: English
      • Number of Pages: Median: 35
      • Publisher: ➤  NASA Scientific and Technical Information Branch - National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
      • Publish Date:
      • Publish Location: ➤  [s.l.] - [Springfield, Va - Washington, D.C

      “Fast euler solver for steady one-dimensional flows” 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

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      6EUROSHOCK

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      “EUROSHOCK” Metadata:

      • Title: EUROSHOCK
      • Authors:
      • Language: English
      • Number of Pages: Median: 414
      • Publisher: ➤  Vieweg - Friedrich Vieweg & Sohn Verlag
      • Publish Date:
      • Publish Location: Braunschweig/Wiesbaden

      “EUROSHOCK” 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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        7A study of canard-wing interference using experimental pressure data at transonic speeds

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        “A study of canard-wing interference using experimental pressure data at transonic speeds” Metadata:

        • Title: ➤  A study of canard-wing interference using experimental pressure data at transonic speeds
        • Author:
        • Language: English
        • Number of Pages: Median: 68
        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
        • Publish Date:
        • Publish Location: [Washington] - Springfield, Va

        “A study of canard-wing interference using experimental pressure data at transonic speeds” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1979
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Marketplaces

        Find A study of canard-wing interference using experimental pressure data at transonic speeds at online marketplaces:


        8Flight-determined stability and control derivatives for the F-111 TACT research aircraft

        By

        “Flight-determined stability and control derivatives for the F-111 TACT research aircraft” Metadata:

        • Title: ➤  Flight-determined stability and control derivatives for the F-111 TACT research aircraft
        • Author:
        • Language: English
        • Number of Pages: Median: 76
        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Service - for sale by the National Technical Information Service
        • Publish Date:
        • Publish Location: [Washington] - Springfield, Va

        “Flight-determined stability and control derivatives for the F-111 TACT research aircraft” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

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

        Online Marketplaces

        Find Flight-determined stability and control derivatives for the F-111 TACT research aircraft at online marketplaces:


        9Wave drag as the objective function in transonic fighter wing optimization

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        “Wave drag as the objective function in transonic fighter wing optimization” Metadata:

        • Title: ➤  Wave drag as the objective function in transonic fighter wing optimization
        • Author:
        • Language: English
        • Number of Pages: Median: 20
        • 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, D.C

        “Wave drag as the objective function in transonic fighter wing optimization” 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

        Find Wave drag as the objective function in transonic fighter wing optimization at online marketplaces:


        10TAS--a transport aircraft/store flow field prediction code

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        “TAS--a transport aircraft/store flow field prediction code” Metadata:

        • Title: ➤  TAS--a transport aircraft/store flow field prediction code
        • Author:
        • Language: English
        • Number of Pages: Median: 50
        • Publisher: ➤  The Center - 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

        “TAS--a transport aircraft/store flow field prediction code” 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 TAS--a transport aircraft/store flow field prediction code at online marketplaces:


        11Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft

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        “Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft” Metadata:

        • Title: ➤  Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft
        • Author:
        • Language: English
        • Number of Pages: Median: 334
        • 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

        “Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft” 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 Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft at online marketplaces:


        12Buffet characteristics of the F-8 supercritical wing airplane

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        “Buffet characteristics of the F-8 supercritical wing airplane” Metadata:

        • Title: ➤  Buffet characteristics of the F-8 supercritical wing airplane
        • Author:
        • Language: English
        • Number of Pages: Median: 29
        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
        • Publish Date:
        • Publish Location: [Washington] - Springfield, Va

        “Buffet characteristics of the F-8 supercritical wing airplane” 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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        13Wing analysis using a transonic potential flow computational method

        By

        “Wing analysis using a transonic potential flow computational method” Metadata:

        • Title: ➤  Wing analysis using a transonic potential flow computational method
        • Author:
        • Language: English
        • Number of Pages: Median: 55
        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
        • Publish Date:
        • Publish Location: [Washington] - Springfield, Va

        “Wing analysis using a transonic potential flow computational method” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

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

        Online Marketplaces

        Find Wing analysis using a transonic potential flow computational method at online marketplaces:


        14Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport

        By

        “Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport” Metadata:

        • Title: ➤  Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport
        • Author:
        • Language: English
        • 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

        “Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport” 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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          Find Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport at online marketplaces:


          15Numerical optimization design of advanced transonic wing configurations

          By

          “Numerical optimization design of advanced transonic wing configurations” Metadata:

          • Title: ➤  Numerical optimization design of advanced transonic wing configurations
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center
          • Publish Date:
          • Publish Location: Moffett Field, Calif

          “Numerical optimization design of advanced transonic wing configurations” 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 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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            16Effect of a variable camber and twist wing at transonic mach numbers

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            “Effect of a variable camber and twist wing at transonic mach numbers” Metadata:

            • Title: ➤  Effect of a variable camber and twist wing at transonic mach numbers
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
            • Publish Date:
            • Publish Location: [Washington, D.C.?]

            “Effect of a variable camber and twist wing at transonic mach numbers” 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 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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              17TAS

              By

              “TAS” Metadata:

              • Title: TAS
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
              • Publish Date:
              • Publish Location: [Washington, D.C.]

              “TAS” 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 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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                18Flight comparison of the transonic agility of the F-111A airplane and the F-111 supercritical wing airplane

                By

                “Flight comparison of the transonic agility of the F-111A airplane and the F-111 supercritical wing airplane” Metadata:

                • Title: ➤  Flight comparison of the transonic agility of the F-111A airplane and the F-111 supercritical wing airplane
                • Author:
                • Language: English
                • Number of Pages: Median: 75
                • 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]

                “Flight comparison of the transonic agility of the F-111A airplane and the F-111 supercritical wing airplane” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

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

                Online Marketplaces

                Find Flight comparison of the transonic agility of the F-111A airplane and the F-111 supercritical wing airplane at online marketplaces:


                19Wave drag as the objective function in transonic fighter wing optimization

                By

                “Wave drag as the objective function in transonic fighter wing optimization” Metadata:

                • Title: ➤  Wave drag as the objective function in transonic fighter wing optimization
                • Author:
                • Language: English
                • Number of Pages: Median: 20
                • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
                • Publish Date:
                • Publish Location: ➤  Washington, D.C - [Springfield, Va

                “Wave drag as the objective function in transonic fighter wing optimization” 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

                Find Wave drag as the objective function in transonic fighter wing optimization at online marketplaces:


                20Transonic airfoil design using cartesian coordinates

                By

                “Transonic airfoil design using cartesian coordinates” Metadata:

                • Title: ➤  Transonic airfoil design using cartesian coordinates
                • Author:
                • Language: English
                • Number of Pages: Median: 33
                • Publisher: ➤  U.S. National Aeronautics and Space Administration - for sale by the National Technical Information Service
                • Publish Date:
                • Publish Location: Washington - Springfield, Va

                “Transonic airfoil design using cartesian coordinates” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1976
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

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