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Source: The Open Library

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1FAR 23 loads

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“FAR 23 loads” Metadata:

  • Title: FAR 23 loads
  • Author:
  • Language: English
  • Number of Pages: Median: 293
  • Publisher: Aero Science Software
  • Publish Date:
  • Publish Location: ➤  [Wichita, Kan.] (7415 Tanglewood Ct., Wichita 67206)

“FAR 23 loads” 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

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2Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing

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“Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing” Metadata:

  • Title: ➤  Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
  • Author:
  • Language: English
  • Number of Pages: Median: 211
  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - Washington, D.C

“Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing” 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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3A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing

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“A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing” Metadata:

  • Title: ➤  A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing
  • Author:
  • Language: English
  • Number of Pages: Median: 51
  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Informaion Branch - For sale by the National Technical Information Service]
  • Publish Date:
  • Publish Location: ➤  Washington, D.C - [Springfield, Va

“A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing” 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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4High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation

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“High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation” Metadata:

  • Title: ➤  High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
  • Author:
  • Language: English
  • Number of Pages: Median: 51
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - [Cleveland, Ohio]

“High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1999
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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    5Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing

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    “Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing” Metadata:

    • Title: ➤  Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
    • Author:
    • Language: English
    • Number of Pages: Median: 193
    • 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 investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing” 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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    6In-flight investigation of shuttle tile pressure orifice installations

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    “In-flight investigation of shuttle tile pressure orifice installations” Metadata:

    • Title: ➤  In-flight investigation of shuttle tile pressure orifice installations
    • Author:
    • Language: English
    • Number of Pages: Median: 33
    • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service - Ames Research Center
    • Publish Date:
    • Publish Location: ➤  Washington, D.C - Springfield, Va - Edwards, Calif

    “In-flight investigation of shuttle tile pressure orifice installations” 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

    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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      7User's guide

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      “User's guide” Metadata:

      • Title: User's guide
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
      • Publish Date:
      • Publish Location: Hampton, Va

      “User's guide” 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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        8F-18 High Alpha Research Vehicle surface pressures

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        “F-18 High Alpha Research Vehicle surface pressures” Metadata:

        • Title: ➤  F-18 High Alpha Research Vehicle surface pressures
        • Author:
        • Language: English
        • Number of Pages: Median: 36
        • Publisher: ➤  National Technical Information Service, distributor] - NASA Ames Resarch Center, Dryden Flight Research Facility
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - Edwards, Calif

        “F-18 High Alpha Research Vehicle surface pressures” 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

        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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          9Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations

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          “Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations” Metadata:

          • Title: ➤  Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations
          • Author:
          • Language: English
          • Number of Pages: Median: 46
          • 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

          “Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations” 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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          10Aircraft dynamic loads due to flow separation

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          “Aircraft dynamic loads due to flow separation” Metadata:

          • Title: ➤  Aircraft dynamic loads due to flow separation
          • Author: ➤  
          • Language: English
          • Number of Pages: Median: 272
          • Publisher: AGARD
          • Publish Date:
          • Publish Location: ➤  Neuilly-sur-Seine - Neuilly sur Seine, France

          “Aircraft dynamic loads due to flow separation” 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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          11Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading

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          “Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading” Metadata:

          • Title: ➤  Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading
          • 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

          “Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading” 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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          12Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations

          By

          “Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations” Metadata:

          • Title: ➤  Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations
          • Author:
          • Language: English
          • Number of Pages: Median: 46
          • 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

          “Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations” 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 Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations at online marketplaces:


          13Fluctuating loads measured on an over-the-wing supersonic jet model

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          “Fluctuating loads measured on an over-the-wing supersonic jet model” Metadata:

          • Title: ➤  Fluctuating loads measured on an over-the-wing supersonic jet model
          • 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]

          “Fluctuating loads measured on an over-the-wing supersonic jet model” 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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          14Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9

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          “Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9” Metadata:

          • Title: ➤  Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9
          • Author:
          • Language: English
          • Number of Pages: Median: 92
          • 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

          “Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9” 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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          Find Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9 at online marketplaces:


          15Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes

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          “Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes” Metadata:

          • Title: ➤  Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes
          • Author:
          • Language: English
          • Number of Pages: Median: 82
          • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
          • Publish Date:
          • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

          “Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes” 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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            16A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft

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            “A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft” Metadata:

            • Title: ➤  A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - For sale by the National Technical Information Service]
            • Publish Date:
            • Publish Location: ➤  [Springfield, Va - Edwards, Calif

            “A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1992
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

            Online Access

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            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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              17Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wing

              By

              “Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wing” Metadata:

              • Title: ➤  Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wing
              • Author:
              • Language: English
              • Number of Pages: Median: 92
              • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Association - for sale by the National Technical Information Service
              • Publish Date:
              • Publish Location: Springfield, Va - [Washington]

              “Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wing” 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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              18Design of a 4-1/2 stage turbine with a stage loading factor of 4.66 and high specific work output

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              “Design of a 4-1/2 stage turbine with a stage loading factor of 4.66 and high specific work output” Metadata:

              • Title: ➤  Design of a 4-1/2 stage turbine with a stage loading factor of 4.66 and high specific work output
              • Author:
              • Language: English
              • Number of Pages: Median: 128
              • Publisher: ➤  U.S. National Aeronautics and Space Administration - for sale by the National Technical Information Service
              • Publish Date:
              • Publish Location: Washington - Springfield, Va

              “Design of a 4-1/2 stage turbine with a stage loading factor of 4.66 and high specific work output” 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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              19Studies on air loads on man

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              “Studies on air loads on man” Metadata:

              • Title: Studies on air loads on man
              • Author:
              • Language: English
              • Publish Date:
              • Publish Location: Oklahoma City, Okla

              “Studies on air loads on man” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1964
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

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              20Some exact calculations of the lift and drag produced by a wedge in supersonic flow

              By

              “Some exact calculations of the lift and drag produced by a wedge in supersonic flow” Metadata:

              • Title: ➤  Some exact calculations of the lift and drag produced by a wedge in supersonic flow
              • Author:
              • Language: English
              • Number of Pages: Median: 17
              • Publisher: H.M.S.O.
              • Publish Date:
              • Publish Location: London

              “Some exact calculations of the lift and drag produced by a wedge in supersonic flow” 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

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              Find Some exact calculations of the lift and drag produced by a wedge in supersonic flow at online marketplaces:


              21The use of load frequency distributions in the specification of design requirements for commercial aircraft

              By

              “The use of load frequency distributions in the specification of design requirements for commercial aircraft” Metadata:

              • Title: ➤  The use of load frequency distributions in the specification of design requirements for commercial aircraft
              • Author:
              • Language: English
              • Number of Pages: Median: 22
              • Publisher: Ministry of Technology
              • Publish Date:
              • Publish Location: Farnborough [Eng.]

              “The use of load frequency distributions in the specification of design requirements for commercial aircraft” 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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              22The pressure distribution at zero lift on a slender delta wing at transonic speeds

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              “The pressure distribution at zero lift on a slender delta wing at transonic speeds” Metadata:

              • Title: ➤  The pressure distribution at zero lift on a slender delta wing at transonic speeds
              • Author:
              • Language: English
              • Number of Pages: Median: 10
              • Publisher: H.M.S.O.
              • Publish Date:
              • Publish Location: London

              “The pressure distribution at zero lift on a slender delta wing at transonic speeds” 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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              23The calculation of the warp to produce a given load and the pressures due to a given thickness on thin slender wings in supersonic flow

              By

              “The calculation of the warp to produce a given load and the pressures due to a given thickness on thin slender wings in supersonic flow” Metadata:

              • Title: ➤  The calculation of the warp to produce a given load and the pressures due to a given thickness on thin slender wings in supersonic flow
              • Author:
              • Language: English
              • Number of Pages: Median: 36
              • Publisher: H.M.S.O.
              • Publish Date:
              • Publish Location: London

              “The calculation of the warp to produce a given load and the pressures due to a given thickness on thin slender wings in supersonic flow” Subjects and Themes:

              Edition Identifiers:

              • The Open Library ID: OL5588302M
              • Online Computer Library Center (OCLC) ID: 6189291
              • Library of Congress Control Number (LCCN): 67108712

              Access and General Info:

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

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              24Manual on aircraft loads

              By

              “Manual on aircraft loads” Metadata:

              • Title: Manual on aircraft loads
              • Author:
              • Language: English
              • Number of Pages: Median: 350
              • Publisher: ➤  Published for and on behalf of Advisory Group for Aeronautical Research and Development, North Atlantic Treaty Organization by Pergamon Press
              • Publish Date:
              • Publish Location: Oxford - New York

              “Manual on aircraft loads” Subjects and Themes:

              Edition Identifiers:

              • The Open Library ID: OL5920835M
              • Online Computer Library Center (OCLC) ID: 1381871
              • Library of Congress Control Number (LCCN): 64024959

              Access and General Info:

              • First Year Published: 1965
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

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              25On the prediction of base pressure on two-dimensional supersonic turbulent flow

              By

              “On the prediction of base pressure on two-dimensional supersonic turbulent flow” Metadata:

              • Title: ➤  On the prediction of base pressure on two-dimensional supersonic turbulent flow
              • Author: ➤  
              • Language: English
              • Number of Pages: Median: 44
              • Publisher: H.M.S.O.
              • Publish Date:
              • Publish Location: London

              “On the prediction of base pressure on two-dimensional supersonic turbulent flow” 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

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              26The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory

              By

              “The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory” Metadata:

              • Title: ➤  The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory
              • Author:
              • Language: English
              • Number of Pages: Median: 43
              • Publisher: H.M.S.O.
              • Publish Date:
              • Publish Location: London

              “The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory” Subjects and Themes:

              Edition Identifiers:

              • The Open Library ID: OL5570853M
              • Online Computer Library Center (OCLC) ID: 6188515
              • Library of Congress Control Number (LCCN): 67078953

              Access and General Info:

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

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              Find The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory at online marketplaces:


              27The estimation of the loading on swept wings with extending chord flaps at subsonic speeds

              By

              “The estimation of the loading on swept wings with extending chord flaps at subsonic speeds” Metadata:

              • Title: ➤  The estimation of the loading on swept wings with extending chord flaps at subsonic speeds
              • Author:
              • Language: English
              • Number of Pages: Median: 30
              • Publisher: H.M. Stationery Off.
              • Publish Date:
              • Publish Location: London

              “The estimation of the loading on swept wings with extending chord flaps at subsonic speeds” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1970
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

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              28The unsteady forces on finite wings in transient motion

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              “The unsteady forces on finite wings in transient motion” Metadata:

              • Title: ➤  The unsteady forces on finite wings in transient motion
              • Author:
              • Language: English
              • Number of Pages: Median: 50
              • Publisher: H.M.S.O.
              • Publish Date:
              • Publish Location: London

              “The unsteady forces on finite wings in transient motion” 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

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              29An analysis of the subsonic flow past symmetrical blunt-trailing-edge aerofoil sections at zero incidence, in the absence of a vortex street

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              “An analysis of the subsonic flow past symmetrical blunt-trailing-edge aerofoil sections at zero incidence, in the absence of a vortex street” Metadata:

              • Title: ➤  An analysis of the subsonic flow past symmetrical blunt-trailing-edge aerofoil sections at zero incidence, in the absence of a vortex street
              • Author:
              • Language: English
              • Number of Pages: Median: 42
              • Publisher: H.M.S.O.
              • Publish Date:
              • Publish Location: London

              “An analysis of the subsonic flow past symmetrical blunt-trailing-edge aerofoil sections at zero incidence, in the absence of a vortex street” Subjects and Themes:

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              • First Year Published: 1966
              • Is Full Text Available: No
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              30The calculation of momentum thickness in a turbulent boundary layer at mach numbers up to unity

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              “The calculation of momentum thickness in a turbulent boundary layer at mach numbers up to unity” Metadata:

              • Title: ➤  The calculation of momentum thickness in a turbulent boundary layer at mach numbers up to unity
              • Author:
              • Language: English
              • Number of Pages: Median: 24
              • Publisher: H.M.S.O.
              • Publish Date:
              • Publish Location: London

              “The calculation of momentum thickness in a turbulent boundary layer at mach numbers up to unity” Subjects and Themes:

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              • First Year Published: 1967
              • Is Full Text Available: No
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              31The use of calibrated strain gauges for flight load determination

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              “The use of calibrated strain gauges for flight load determination” Metadata:

              • Title: ➤  The use of calibrated strain gauges for flight load determination
              • Author:
              • Language: English
              • Number of Pages: Median: 21
              • Publisher: H.M.S.O.
              • Publish Date:
              • Publish Location: London

              “The use of calibrated strain gauges for flight load determination” Subjects and Themes:

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              • First Year Published: 1969
              • Is Full Text Available: No
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              32Theoretical and experimental vibration and buckling results for blunt truncated conical shells with ring-supported edges

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              “Theoretical and experimental vibration and buckling results for blunt truncated conical shells with ring-supported edges” Metadata:

              • Title: ➤  Theoretical and experimental vibration and buckling results for blunt truncated conical shells with ring-supported edges
              • Author:
              • Language: English
              • Number of Pages: Median: 32
              • Publisher: ➤  National Aeronautics and Space Administration; [for sale by the National Technical Information Service, Springfield, Va.]
              • Publish Date:
              • Publish Location: Washington

              “Theoretical and experimental vibration and buckling results for blunt truncated conical shells with ring-supported edges” Subjects and Themes:

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              • First Year Published: 1970
              • Is Full Text Available: No
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              33Boundary layer effects on unsteady airloads

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              “Boundary layer effects on unsteady airloads” Metadata:

              • Title: ➤  Boundary layer effects on unsteady airloads
              • Author: ➤  
              • Language: English
              • Number of Pages: Median: 173
              • Publisher: ➤  North Atlantic Treaty Organization, Advisory Group for Aerospace Research & Development
              • Publish Date:
              • Publish Location: Neuilly sur Seine, France

              “Boundary layer effects on unsteady airloads” Subjects and Themes:

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              • First Year Published: 1981
              • Is Full Text Available: No
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              34Unsteady airloads in separated and transonic flow

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              “Unsteady airloads in separated and transonic flow” Metadata:

              • Title: ➤  Unsteady airloads in separated and transonic flow
              • Author: ➤  
              • Language: English
              • Number of Pages: Median: 271
              • Publisher: ➤  North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development
              • Publish Date:
              • Publish Location: Neuilly-sur-Seine, France

              “Unsteady airloads in separated and transonic flow” Subjects and Themes:

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              • First Year Published: 1977
              • Is Full Text Available: No
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              35Agricultural aircraft flight loads

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              “Agricultural aircraft flight loads” Metadata:

              • Title: ➤  Agricultural aircraft flight loads
              • Author:
              • Language: English
              • Number of Pages: Median: 16
              • Publisher: ➤  Dept. of Supply, Australian Defence Scientific Service, Aeronautical Research Laboratories
              • Publish Date:
              • Publish Location: Melbourne

              “Agricultural aircraft flight loads” Subjects and Themes:

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

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              36Aerodynamic force analysis

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              “Aerodynamic force analysis” Metadata:

              • Title: Aerodynamic force analysis
              • Author:
              • Language: English
              • Publish Date:
              • Publish Location: [Auburn?, Ala.]

              “Aerodynamic force analysis” Subjects and Themes:

              Edition Identifiers:

              • The Open Library ID: OL5561185M
              • Online Computer Library Center (OCLC) ID: 1200879
              • Library of Congress Control Number (LCCN): 67060915

              Access and General Info:

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

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              37CCBLADE documentation

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              “CCBLADE documentation” Metadata:

              • Title: CCBLADE documentation
              • Author:
              • Language: English
              • Number of Pages: Median: 23
              • Publisher: ➤  National Renewable Energy Laboratory
              • Publish Date:
              • Publish Location: Golden, CO

              “CCBLADE documentation” Subjects and Themes:

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              • First Year Published: 2013
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

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              38Allocating variability and reserve requirements

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              “Allocating variability and reserve requirements” Metadata:

              • Title: ➤  Allocating variability and reserve requirements
              • Author:
              • Language: English
              • Number of Pages: Median: 13
              • Publisher: ➤  National Renewable Energy Laboratory
              • Publish Date:
              • Publish Location: Golden, Colo.]

              “Allocating variability and reserve requirements” Subjects and Themes:

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              • First Year Published: 2011
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

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                39Druckverteilungsmessungen an Keilen bei Unterschall- und Transschallgeschwindigkeiten

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                “Druckverteilungsmessungen an Keilen bei Unterschall- und Transschallgeschwindigkeiten” Metadata:

                • Title: ➤  Druckverteilungsmessungen an Keilen bei Unterschall- und Transschallgeschwindigkeiten
                • Author:
                • Language: ger
                • Number of Pages: Median: 57
                • Publisher: ➤  Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt - Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt
                • Publish Date:
                • Publish Location: Köln

                “Druckverteilungsmessungen an Keilen bei Unterschall- und Transschallgeschwindigkeiten” Subjects and Themes:

                Edition Identifiers:

                • The Open Library ID: OL2653513M
                • Online Computer Library Center (OCLC) ID: 19556471
                • Library of Congress Control Number (LCCN): 85236339

                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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                40Aircraft loading and structural layout

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                Book's cover

                “Aircraft loading and structural layout” Metadata:

                • Title: ➤  Aircraft loading and structural layout
                • Author:
                • Language: English
                • Number of Pages: Median: 591
                • Publisher: ➤  American Institute of Aeronautics and Astronautics
                • Publish Date:
                • Publish Location: Reston, VA

                “Aircraft loading and structural layout” Subjects and Themes:

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                • First Year Published: 2004
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

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                41A method for the prediction of wing response to nonstationary buffet loads =

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                “A method for the prediction of wing response to nonstationary buffet loads =” Metadata:

                • Title: ➤  A method for the prediction of wing response to nonstationary buffet loads =
                • Author:
                • Language: English
                • Number of Pages: Median: 69
                • Publisher: ➤  National Research Council Canada
                • Publish Date:
                • Publish Location: Ottawa, Ont

                “A method for the prediction of wing response to nonstationary buffet loads =” Subjects and Themes:

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                • First Year Published: 1980
                • Is Full Text Available: No
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                42Aircraft loading actions problems--proceedings of a symposium held at Farnborough on 28th October 1966

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                “Aircraft loading actions problems--proceedings of a symposium held at Farnborough on 28th October 1966” Metadata:

                • Title: ➤  Aircraft loading actions problems--proceedings of a symposium held at Farnborough on 28th October 1966
                • Authors:
                • Language: English
                • Number of Pages: Median: 182
                • Publisher: H.M. Stationery Off.
                • Publish Date:
                • Publish Location: London

                “Aircraft loading actions problems--proceedings of a symposium held at Farnborough on 28th October 1966” Subjects and Themes:

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                • First Year Published: 1968
                • Is Full Text Available: No
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                43Chi xu zai he fei xing fang zhen ji shu yu gong cheng she ji

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                “Chi xu zai he fei xing fang zhen ji shu yu gong cheng she ji” Metadata:

                • Title: ➤  Chi xu zai he fei xing fang zhen ji shu yu gong cheng she ji
                • Author:
                • Language: chi
                • Number of Pages: Median: 292
                • Publisher: Guo fang gong ye chu ban she
                • Publish Date:
                • Publish Location: Beijing

                “Chi xu zai he fei xing fang zhen ji shu yu gong cheng she ji” Subjects and Themes:

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                • First Year Published: 2013
                • Is Full Text Available: No
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                44Fei ji jie gou zai he, huan jing pu

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                “Fei ji jie gou zai he, huan jing pu” Metadata:

                • Title: ➤  Fei ji jie gou zai he, huan jing pu
                • Author:
                • Language: chi
                • Number of Pages: Median: 400
                • Publisher: Dian zi gong ye chu ban she
                • Publish Date:
                • Publish Location: Beijing Shi

                “Fei ji jie gou zai he, huan jing pu” Subjects and Themes:

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                • First Year Published: 2012
                • Is Full Text Available: No
                • Is The Book Public: No
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                45Regional incidence of CAT and the meteorological interpretation of routine flight load records

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                “Regional incidence of CAT and the meteorological interpretation of routine flight load records” Metadata:

                • Title: ➤  Regional incidence of CAT and the meteorological interpretation of routine flight load records
                • Author:
                • Language: English
                • Number of Pages: Median: 38
                • Publisher: ➤  Dept. of the Interior. Bureau of Meteorology
                • Publish Date:
                • Publish Location: [Canberra]

                “Regional incidence of CAT and the meteorological interpretation of routine flight load records” Subjects and Themes:

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                • First Year Published: 1971
                • Is Full Text Available: No
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                46Sergio Adrián Pérez

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                “Sergio Adrián Pérez” Metadata:

                • Title: Sergio Adrián Pérez
                • Author:
                • Language: English
                • Publisher: ➤  Institute for Aerospace Studies, University of Toronto
                • Publish Date:
                • Publish Location: Downsview, Ont

                “Sergio Adrián Pérez” Subjects and Themes:

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                • First Year Published: 1990
                • Is Full Text Available: No
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                47Application of numerical integration techniques to the low-aspect-ratio flutter problem in subsonic and supersonic flows

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                “Application of numerical integration techniques to the low-aspect-ratio flutter problem in subsonic and supersonic flows” Metadata:

                • Title: ➤  Application of numerical integration techniques to the low-aspect-ratio flutter problem in subsonic and supersonic flows
                • Author:
                • Language: English
                • Number of Pages: Median: 195
                • Publisher: ➤  Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, Aero-Elastic and Structures Research
                • Publish Date:
                • Publish Location: [Cambridge, Mass.]

                “Application of numerical integration techniques to the low-aspect-ratio flutter problem in subsonic and supersonic flows” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1954
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

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                48Parametric study of afterbody/nozzle drag on twin two-dimensional convergent-divergent nozzles at mach numbers from 0.60 to 1.20

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                “Parametric study of afterbody/nozzle drag on twin two-dimensional convergent-divergent nozzles at mach numbers from 0.60 to 1.20” Metadata:

                • Title: ➤  Parametric study of afterbody/nozzle drag on twin two-dimensional convergent-divergent nozzles at mach numbers from 0.60 to 1.20
                • Author:
                • Language: English
                • Publisher: ➤  National Technical Information Service [distributor] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
                • Publish Date:
                • Publish Location: ➤  [Washington, DC] - [Springfield, Va.?

                “Parametric study of afterbody/nozzle drag on twin two-dimensional convergent-divergent nozzles at mach numbers from 0.60 to 1.20” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1986
                • Is Full Text Available: No
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                • Access Status: No_ebook

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                  49Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing

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                  “Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing” Metadata:

                  • Title: ➤  Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
                  • Author:
                  • Language: English
                  • Number of Pages: Median: 175
                  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
                  • Publish Date:
                  • Publish Location: ➤  [Springfield, Va - Washington, D.C

                  “Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing” Subjects and Themes:

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                  • First Year Published: 1983
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

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                  50Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9

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                  “Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9” Metadata:

                  • Title: ➤  Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9
                  • 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

                  “Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9” Subjects and Themes:

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                  • First Year Published: 1983
                  • Is Full Text Available: No
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