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Source: The Open Library

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1In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)

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“In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)” Metadata:

  • Title: ➤  In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - [Washington, DC]

“In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)” 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

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    2Optimum shape of a blunt forebody in hypersonic flow

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    “Optimum shape of a blunt forebody in hypersonic flow” Metadata:

    • Title: ➤  Optimum shape of a blunt forebody in hypersonic flow
    • Author:
    • Language: English
    • Publisher: NASA Langley Research Center
    • Publish Date:
    • Publish Location: Hampton, Va

    “Optimum shape of a blunt forebody in hypersonic flow” 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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      3Wave drag determination in the transonic full-potential flow code matrics

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      “Wave drag determination in the transonic full-potential flow code matrics” Metadata:

      • Title: ➤  Wave drag determination in the transonic full-potential flow code matrics
      • Author:
      • Number of Pages: Median: 29
      • Publisher: National Aerospace Laboratory
      • Publish Date:
      • Publish Location: Amsterdam

      “Wave drag determination in the transonic full-potential flow code matrics” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1990
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

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      4Aerothermal performance constraints for hypervelocity small radius unswept leading edges and nosetips

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      “Aerothermal performance constraints for hypervelocity small radius unswept leading edges and nosetips” Metadata:

      • Title: ➤  Aerothermal performance constraints for hypervelocity small radius unswept leading edges and nosetips
      • 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

      “Aerothermal performance constraints for hypervelocity small radius unswept leading edges and nosetips” 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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        Wiki

        Source: Wikipedia

        Wikipedia Results

        Search Results from Wikipedia

        Wave drag

        In aeronautics, wave drag is a component of the aerodynamic drag on aircraft wings and fuselage, propeller blade tips and projectiles moving at transonic

        Drag (physics)

        of categorizing drag. Pressure drag and friction drag Profile drag and induced drag Vortex drag, wave drag and wake drag The pressure distribution acting

        Parasitic drag

        Parasitic drag, also known as profile drag, is a type of aerodynamic drag that acts on any object when the object is moving through a fluid. Parasitic drag is

        Area rule

        waves formed at these zones of sonic flow cause a sudden increase in drag, called wave drag. To reduce the number and strength of these shock waves,

        Supercritical airfoil

        British English) is an airfoil designed primarily to delay the onset of wave drag in the transonic speed range. Supercritical airfoils are characterized

        Shock wave

        extracted as work, and as a drag force on supersonic objects; shock waves are strongly irreversible processes. Shock waves can be: Normal At 90° (perpendicular)

        Transonic

        increase in drag from about Mach 0.8, and it is the fuel costs of the drag that typically limits the airspeed. Attempts to reduce wave drag can be seen

        Wave-making resistance

        Wave-making resistance or wave resistance is a form of drag that affects any object moving on a surface of a fluid, such as boats and ships moving on

        Busemann biplane

        which avoids the formation of N-type shock waves and thus does not create a sonic boom or the associated wave drag. However in its original form it does not

        Sears–Haack body

        The Sears–Haack body is the shape with the lowest theoretical wave drag in supersonic flow, for a slender solid body of revolution with a given body length