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Source: The Open Library

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1Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control

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“Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control” Metadata:

  • Title: ➤  Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control
  • Author:
  • Language: English
  • Number of Pages: Median: 101
  • 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

“Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control” 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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2Pseudosteady-state analysis of nonlinear aircraft maneuvers

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“Pseudosteady-state analysis of nonlinear aircraft maneuvers” Metadata:

  • Title: ➤  Pseudosteady-state analysis of nonlinear aircraft maneuvers
  • Author:
  • Language: English
  • Number of Pages: Median: 61
  • 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

“Pseudosteady-state analysis of nonlinear aircraft maneuvers” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1980
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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3Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control

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“Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control” Metadata:

  • Title: ➤  Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control
  • Author:
  • Language: English
  • Number of Pages: Median: 101
  • 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

“Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control” 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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4Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds

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“Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds” Metadata:

  • Title: ➤  Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds
  • Author:
  • Language: English
  • Number of Pages: Median: 197
  • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - Washington, D.C

“Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1980
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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5The roll control of magnetically suspended wind tunnel models by transverse magnets

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“The roll control of magnetically suspended wind tunnel models by transverse magnets” Metadata:

  • Title: ➤  The roll control of magnetically suspended wind tunnel models by transverse magnets
  • Author:
  • Language: English
  • Number of Pages: Median: 19
  • Publisher: ➤  University ofSouthampton. Department of Aeronautics and Astronautics - Dept. of Aeronautics and Astronautics, University
  • Publish Date:
  • Publish Location: ➤  Southampton, [Eng.] - Southampton

“The roll control of magnetically suspended wind tunnel models by transverse magnets” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1968
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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6A simulator investigation of rolling requirements for landing approach

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“A simulator investigation of rolling requirements for landing approach” Metadata:

  • Title: ➤  A simulator investigation of rolling requirements for landing approach
  • Author:
  • Language: English
  • Number of Pages: Median: 37
  • Publisher: H.M. Stationery Off.
  • Publish Date:
  • Publish Location: London

“A simulator investigation of rolling requirements for landing approach” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1969
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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7Theoretical study of the rolling response of aircraft to turbulent air

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“Theoretical study of the rolling response of aircraft to turbulent air” Metadata:

  • Title: ➤  Theoretical study of the rolling response of aircraft to turbulent air
  • Author:
  • Language: English
  • Number of Pages: Median: 31
  • Publisher: H.M.S.O.
  • Publish Date:
  • Publish Location: London

“Theoretical study of the rolling response of aircraft to turbulent air” Subjects and Themes:

Edition Identifiers:

  • The Open Library ID: OL5568371M
  • Online Computer Library Center (OCLC) ID: 6184103
  • Library of Congress Control Number (LCCN): 67074993

Access and General Info:

  • First Year Published: 1966
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

Online Marketplaces

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8A simulation approach to estimate the efficacy of meritor WABCO's improved roll stability control

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“A simulation approach to estimate the efficacy of meritor WABCO's improved roll stability control” Metadata:

  • Title: ➤  A simulation approach to estimate the efficacy of meritor WABCO's improved roll stability control
  • Author:
  • Language: English
  • Number of Pages: Median: 42
  • Publisher: ➤  U.S. Department of Transportation, Federal Motor Carrier Safety Administration
  • Publish Date:
  • Publish Location: Washington, DC

“A simulation approach to estimate the efficacy of meritor WABCO's improved roll stability control” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 2006
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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9Lateral rollover protection concepts

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“Lateral rollover protection concepts” Metadata:

  • Title: ➤  Lateral rollover protection concepts
  • Author:
  • Language: English
  • Number of Pages: Median: 106
  • Publisher: The Laboratory
  • Publish Date:
  • Publish Location: Fort Eustis, Va

“Lateral rollover protection concepts” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1980
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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10Semiempirical method for predicting vortex-induced rolling moments

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“Semiempirical method for predicting vortex-induced rolling moments” Metadata:

  • Title: ➤  Semiempirical method for predicting vortex-induced rolling moments
  • Author:
  • Language: English
  • Number of Pages: Median: 16
  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
  • Publish Date:
  • Publish Location: [Washington, D.C.]

“Semiempirical method for predicting vortex-induced rolling moments” 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

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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    11Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds

    By

    “Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds” Metadata:

    • Title: ➤  Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds
    • Author:
    • Language: English
    • Number of Pages: Median: 197
    • 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

    “Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1980
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Marketplaces

    Find Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds at online marketplaces:


    12Numerical study of transonic flow over oscillating airfoils using the full potential equation

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    “Numerical study of transonic flow over oscillating airfoils using the full potential equation” Metadata:

    • Title: ➤  Numerical study of transonic flow over oscillating airfoils using the full potential equation
    • Author:
    • Language: English
    • Number of Pages: Median: 38
    • 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

    “Numerical study of transonic flow over oscillating airfoils using the full potential equation” 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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    13Computer programs for calculation of sting pitch and roll angles required to obtain angles of attack and sideslip on wind tunnel models

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    “Computer programs for calculation of sting pitch and roll angles required to obtain angles of attack and sideslip on wind tunnel models” Metadata:

    • Title: ➤  Computer programs for calculation of sting pitch and roll angles required to obtain angles of attack and sideslip on wind tunnel models
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
    • Publish Date:
    • Publish Location: Hampton, Va - [Springfield, Va

    “Computer programs for calculation of sting pitch and roll angles required to obtain angles of attack and sideslip on wind tunnel models” 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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      14Computer programs for the calculation of dual sting pitch and roll angles required for an articulated sting to obtain angles of attack and sideslip on wind-tunnel models

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      “Computer programs for the calculation of dual sting pitch and roll angles required for an articulated sting to obtain angles of attack and sideslip on wind-tunnel models” Metadata:

      • Title: ➤  Computer programs for the calculation of dual sting pitch and roll angles required for an articulated sting to obtain angles of attack and sideslip on wind-tunnel models
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
      • Publish Date:
      • Publish Location: Hampton, Va - [Springfield, Va

      “Computer programs for the calculation of dual sting pitch and roll angles required for an articulated sting to obtain angles of attack and sideslip on wind-tunnel models” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1991
      • 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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        15Design considerations of manipulator and feel system characteristics in roll tracking

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        “Design considerations of manipulator and feel system characteristics in roll tracking” Metadata:

        • Title: ➤  Design considerations of manipulator and feel system characteristics in roll tracking
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Division
        • Publish Date:
        • Publish Location: [Washington, D.C.]

        “Design considerations of manipulator and feel system characteristics in roll tracking” 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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          16Measurements of the rolling response of a fighter aeroplane (Hunter Mk.6) to turbulent air and a comparison with theory

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          “Measurements of the rolling response of a fighter aeroplane (Hunter Mk.6) to turbulent air and a comparison with theory” Metadata:

          • Title: ➤  Measurements of the rolling response of a fighter aeroplane (Hunter Mk.6) to turbulent air and a comparison with theory
          • Author:
          • Language: English
          • Publisher: H.M.S.O.
          • Publish Date:
          • Publish Location: London

          “Measurements of the rolling response of a fighter aeroplane (Hunter Mk.6) to turbulent air and a comparison with theory” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1966
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Marketplaces

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          17An investigation of the rolling moments due to side-slip on high tailplanes

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          “An investigation of the rolling moments due to side-slip on high tailplanes” Metadata:

          • Title: ➤  An investigation of the rolling moments due to side-slip on high tailplanes
          • Author:
          • Language: English
          • Number of Pages: Median: 21
          • Publisher: H.M.S.O.
          • Publish Date:
          • Publish Location: London

          “An investigation of the rolling moments due to side-slip on high tailplanes” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1968
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Marketplaces

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          18The generation of rolling moments with the superconducting solenoid model

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          “The generation of rolling moments with the superconducting solenoid model” Metadata:

          • Title: ➤  The generation of rolling moments with the superconducting solenoid model
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
          • Publish Date:
          • Publish Location: Hampton, Va

          “The generation of rolling moments with the superconducting solenoid model” 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

          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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