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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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    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

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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:

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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

      By

      “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

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

        By

        “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

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        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

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        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

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

        By

        “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

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        12Buffet characteristics of the F-8 supercritical wing airplane

        By

        “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

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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

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        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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          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.

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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

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                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

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                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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                Wiki

                Source: Wikipedia

                Wikipedia Results

                Search Results from Wikipedia

                Transonic

                Transonic (or transsonic) flow is air flowing around an object at a speed that generates regions of both subsonic and supersonic airflow around that object

                List of X-planes

                have also since sponsored X-plane projects. The first experimental aircraft specification, for a transonic rocket plane, was placed in 1945, and the

                Airplane

                that of smaller private planes, with the per-mile statistic indicating that airliners are 8.3 times safer than smaller planes. Like all activities involving

                Swept wing

                Wings: Convair's High-Speed Planes of the Fifties and Sixties. Motorbooks. 1983. Myhra, David. Focke-Wulf Ta 183 (X Planes of the Third Reich). Atglen

                Area rule

                Whitcomb and also called the transonic area rule, is a design procedure used to reduce an aircraft's drag at transonic speeds which occur between about

                Sound barrier

                reliable in the transonic. Further, a series of tests made by Karl Doetsch at the behest of Willy Messerschmitt found that the plane became uncontrollable

                Tailplane

                tail planes of the old Farman biplanes were "lifting tail planes," and were, as a matter of fact, rather heavily cambered. By a non-lifting tail plane is

                Boeing X-66

                11 ft (3.4 m) transonic tunnel, then later in 2019 at the 14 by 22 ft (4.3 by 6.7 m) subsonic tunnel at NASA Langley. A full-scale X-plane is being developed

                Boeing Truss-Braced Wing

                "NASA Picks Boeing's Transonic Truss-Based Wing For Sustainable X-Plane". Aviation Week. "Boeing producing battery-powered hybrid plane". Northwest Cable

                Mach number

                categories:[citation needed] At transonic speeds, the flow field around the object includes both sub- and supersonic parts. The transonic period begins when first