Explore: Ground Simulators

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Source: The Open Library

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1Wind-tunnel test of an articulated helicopter rotor model with several tip shapes

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“Wind-tunnel test of an articulated helicopter rotor model with several tip shapes” Metadata:

  • Title: ➤  Wind-tunnel test of an articulated helicopter rotor model with several tip shapes
  • Author:
  • Language: English
  • Number of Pages: Median: 92
  • Publisher: ➤  Fo r sale by the National Technical Information Service] - National Aeronautics and Space Administrat ion, Scientific and Technical Information Branch
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - Washington, D.C

“Wind-tunnel test of an articulated helicopter rotor model with several tip shapes” 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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2The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models

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“The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models” Metadata:

  • Title: ➤  The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models
  • Author:
  • Language: English
  • Publisher: ➤  Flight Research Laboratory, University of Kansas, Center for Research Inc.
  • Publish Date:
  • Publish Location: Lawrence, Kan

“The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models” 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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    3Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8êto 90ê

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    “Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8êto 90ê” Metadata:

    • Title: ➤  Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8êto 90ê
    • Author:
    • Language: English
    • Number of Pages: Median: 692
    • 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

    “Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8êto 90ê” 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

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    4Performance testing of a main rotor system for a utility helicopter at 1/4 scale

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    “Performance testing of a main rotor system for a utility helicopter at 1/4 scale” Metadata:

    • Title: ➤  Performance testing of a main rotor system for a utility helicopter at 1/4 scale
    • Author:
    • Language: English
    • Number of Pages: Median: 45
    • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - Washington, D.C

    “Performance testing of a main rotor system for a utility helicopter at 1/4 scale” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1982
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Marketplaces

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    5Advanced hypersonic test facilities

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    Book's cover

    “Advanced hypersonic test facilities” Metadata:

    • Title: ➤  Advanced hypersonic test facilities
    • Author:
    • Language: English
    • Number of Pages: Median: 632
    • Publisher: ➤  AIAA (American Institute of Aeronautics & Ast - AIAA - American Institute of Aeronautics and Astronautics - AIAA (American Institute of Aeronautics & Astronautics)
    • Publish Date:
    • Publish Location: Reston, Va

    “Advanced hypersonic test facilities” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 2002
    • 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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      6Wind-tunnel test of an articlulated helicopter rotor model with several tip shapes

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      “Wind-tunnel test of an articlulated helicopter rotor model with several tip shapes” Metadata:

      • Title: ➤  Wind-tunnel test of an articlulated helicopter rotor model with several tip shapes
      • Author:
      • Language: English
      • Number of Pages: Median: 92
      • 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

      “Wind-tunnel test of an articlulated helicopter rotor model with several tip shapes” 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 Wind-tunnel test of an articlulated helicopter rotor model with several tip shapes at online marketplaces:


      7Applications and requirements for real-time simulators in ground-test facilities

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      “Applications and requirements for real-time simulators in ground-test facilities” Metadata:

      • Title: ➤  Applications and requirements for real-time simulators in ground-test facilities
      • Author:
      • Language: English
      • Number of Pages: Median: 23
      • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - Lewis Research Center - For sale by the National Technical Information Service]
      • Publish Date:
      • Publish Location: ➤  Cleveland, Ohio - [Springfield, Va - [Washington, D.C.]

      “Applications and requirements for real-time simulators in ground-test facilities” 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

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        8Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90[ANG]

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        “Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90[ANG]” Metadata:

        • Title: ➤  Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90[ANG]
        • Author:
        • Language: English
        • Number of Pages: Median: 220
        • 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

        “Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90[ANG]” 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 Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90[ANG] at online marketplaces:


        9Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊

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        “Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊” Metadata:

        • Title: ➤  Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊
        • Author:
        • Language: English
        • Number of Pages: Median: 692
        • 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

        “Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊” 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 Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊ at online marketplaces:


        10A moving-belt rig for ground simulation in low-speed wind tunnels

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        “A moving-belt rig for ground simulation in low-speed wind tunnels” Metadata:

        • Title: ➤  A moving-belt rig for ground simulation in low-speed wind tunnels
        • Author:
        • Language: English
        • Number of Pages: Median: 19
        • Publisher: H.M.S.O.
        • Publish Date:
        • Publish Location: London

        “A moving-belt rig for ground simulation in low-speed wind tunnels” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1967
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Marketplaces

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        11Die Verdrängungskorrekturen in Unterschallwindkanälen bei sperrigen Modellen und mit Bodensimulation

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        “Die Verdrängungskorrekturen in Unterschallwindkanälen bei sperrigen Modellen und mit Bodensimulation” Metadata:

        • Title: ➤  Die Verdrängungskorrekturen in Unterschallwindkanälen bei sperrigen Modellen und mit Bodensimulation
        • Author:
        • Language: ger
        • Number of Pages: Median: 119
        • Publisher: ➤  Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt, Zentralabteilung Niedergeschwindigkeits-Windkanäle
        • Publish Date:
        • Publish Location: Porz-Wahn

        “Die Verdrängungskorrekturen in Unterschallwindkanälen bei sperrigen Modellen und mit Bodensimulation” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1974
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Marketplaces

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        12Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests

        By

        “Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests” Metadata:

        • Title: ➤  Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests
        • Author:
        • Language: English
        • Number of Pages: Median: 33
        • 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

        “Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests” 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 Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests at online marketplaces:


        13Performance testing of a main rotor system for a utility helicopter at 1/4 scale

        By

        “Performance testing of a main rotor system for a utility helicopter at 1/4 scale” Metadata:

        • Title: ➤  Performance testing of a main rotor system for a utility helicopter at 1/4 scale
        • Author:
        • Language: English
        • Number of Pages: Median: 45
        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Scientific and Technical Information Branch
        • Publish Date:
        • Publish Location: ➤  Washington, D.C - [Springfield, Va

        “Performance testing of a main rotor system for a utility helicopter at 1/4 scale” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1982
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Marketplaces

        Find Performance testing of a main rotor system for a utility helicopter at 1/4 scale at online marketplaces:


        14A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel

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        “A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel” Metadata:

        • Title: ➤  A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel
        • Author:
        • Language: English
        • Number of Pages: Median: 18
        • 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

        “A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel” 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

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        15Wind tunnel measurements in the wakes of structures

        By

        “Wind tunnel measurements in the wakes of structures” Metadata:

        • Title: ➤  Wind tunnel measurements in the wakes of structures
        • Author:
        • Language: English
        • Number of Pages: Median: 226
        • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration
        • Publish Date:
        • Publish Location: Washington - Springfield, Va

        “Wind tunnel measurements in the wakes of structures” 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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        16Wind tunnel simulation and field measurements of flow over a coastal headland

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        “Wind tunnel simulation and field measurements of flow over a coastal headland” Metadata:

        • Title: ➤  Wind tunnel simulation and field measurements of flow over a coastal headland
        • Author:
        • Language: English
        • Number of Pages: Median: 158
        • Publish Date:

        “Wind tunnel simulation and field measurements of flow over a coastal headland” 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

        Online Marketplaces

        Find Wind tunnel simulation and field measurements of flow over a coastal headland at online marketplaces:


        17Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8êto 90[ANG]

        By

        “Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8êto 90[ANG]” Metadata:

        • Title: ➤  Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8êto 90[ANG]
        • Author:
        • Language: English
        • Number of Pages: Median: 220
        • 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

        “Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8êto 90[ANG]” 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 Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8êto 90[ANG] at online marketplaces:


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