Explore: Missile Configurations

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Source: The Open Library

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1Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds

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“Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” Metadata:

  • Title: ➤  Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds
  • Author:
  • Language: English
  • Number of Pages: Median: 115
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
  • Publish Date:
  • Publish Location: Hampton, Va - [Springfield, Va

“Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” 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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    2Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds

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    “Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds” Metadata:

    • Title: ➤  Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
    • Publish Date:
    • Publish Location: Hampton, Va

    “Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds” 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:

      Online Marketplaces

      Find Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds at online marketplaces:


      3Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails

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      “Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails” Metadata:

      • Title: ➤  Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: [Springfield, Va - Hampton, Va

      “Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails” 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:

      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:

        Online Marketplaces

        Find Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails at online marketplaces: