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Source: The Open Library

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1Development of in-fiber reflective Bragg gratings as shear stress monitors in aerodynamic facilities

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“Development of in-fiber reflective Bragg gratings as shear stress monitors in aerodynamic facilities” Metadata:

  • Title: ➤  Development of in-fiber reflective Bragg gratings as shear stress monitors in aerodynamic facilities
  • Author:
  • Language: English
  • Number of Pages: Median: 16
  • Publisher: ➤  National Technical Information Service, distributor - Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
  • Publish Date:
  • Publish Location: Hampton, Va - Springfield, VA

“Development of in-fiber reflective Bragg gratings as shear stress monitors in aerodynamic facilities” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1998
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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    2Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction

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    “Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction” Metadata:

    • Title: ➤  Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction
    • Author: ➤  
    • Language: English
    • Publisher: ➤  American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  Springfield, Va - Washington, D.C

    “Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1994
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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      3Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows

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      “Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows” Metadata:

      • Title: ➤  Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: Hampton, Va - [Springfield, Va

      “Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1995
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

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        4Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique

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        “Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique” Metadata:

        • Title: ➤  Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  [Washington, DC - Springfield, Va

        “Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1993
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

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          5Instrumentation development for study of Reynolds analogy in reacting flows

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          “Instrumentation development for study of Reynolds analogy in reacting flows” Metadata:

          • Title: ➤  Instrumentation development for study of Reynolds analogy in reacting flows
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: [Springfield, Va - Hampton, Va

          “Instrumentation development for study of Reynolds analogy in reacting flows” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1995
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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            6Shock tunnel studies of scramjet phenomena 1994

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            “Shock tunnel studies of scramjet phenomena 1994” Metadata:

            • Title: ➤  Shock tunnel studies of scramjet phenomena 1994
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
            • Publish Date:
            • Publish Location: Hampton, Va - [Springfield, Va

            “Shock tunnel studies of scramjet phenomena 1994” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1997
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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              7Shock tunnel studies of scramjet phenomena 1995

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              “Shock tunnel studies of scramjet phenomena 1995” Metadata:

              • Title: ➤  Shock tunnel studies of scramjet phenomena 1995
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: Hampton, Va - [Springfield, Va

              “Shock tunnel studies of scramjet phenomena 1995” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1997
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

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                8Feasibility of generating an "artificial" burst in a turbulent boundary layer

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                “Feasibility of generating an "artificial" burst in a turbulent boundary layer” Metadata:

                • Title: ➤  Feasibility of generating an "artificial" burst in a turbulent boundary layer
                • Author:
                • Number of Pages: Median: 90
                • Publisher: Langley Research Center
                • Publish Date:
                • Publish Location: Hampton, Va

                “Feasibility of generating an "artificial" burst in a turbulent boundary layer” 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

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                9Evaluation of heated film sensors for the measurement of wall shear stress

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                “Evaluation of heated film sensors for the measurement of wall shear stress” Metadata:

                • Title: ➤  Evaluation of heated film sensors for the measurement of wall shear stress
                • Author:
                • Number of Pages: Median: 47
                • Publisher: ➤  Dept. of Aerospace Science and Engineering
                • Publish Date:
                • Publish Location: [Toronto, Ont.]

                “Evaluation of heated film sensors for the measurement of wall shear stress” 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

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                10Analysis and evaluation of an integrated laminar flow control propulsion system

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                “Analysis and evaluation of an integrated laminar flow control propulsion system” Metadata:

                • Title: ➤  Analysis and evaluation of an integrated laminar flow control propulsion system
                • Author:
                • Language: English
                • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                • Publish Date:
                • Publish Location: ➤  Springfield, Va - [Washington, DC

                “Analysis and evaluation of an integrated laminar flow control propulsion system” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1993
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

                Online Access

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                  11An analysis code for the Rapid Engineering Estimation of Momentum and Energy Losses (REMEL)

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                  “An analysis code for the Rapid Engineering Estimation of Momentum and Energy Losses (REMEL)” Metadata:

                  • Title: ➤  An analysis code for the Rapid Engineering Estimation of Momentum and Energy Losses (REMEL)
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                  • Publish Date:
                  • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                  “An analysis code for the Rapid Engineering Estimation of Momentum and Energy Losses (REMEL)” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1994
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

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                    12Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport

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                    “Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport” Metadata:

                    • Title: ➤  Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport
                    • Author:
                    • Language: English
                    • 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

                    “Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport” 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

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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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                      13Hydrodynamic aspects of shark scales

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                      “Hydrodynamic aspects of shark scales” Metadata:

                      • Title: ➤  Hydrodynamic aspects of shark scales
                      • Author:
                      • Language: English
                      • Number of Pages: Median: 110
                      • 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.]

                      “Hydrodynamic aspects of shark scales” 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

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                        14A method for the approximate calculation of the skin friction coefficient of horizontal wavy plates

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                        “A method for the approximate calculation of the skin friction coefficient of horizontal wavy plates” Metadata:

                        • Title: ➤  A method for the approximate calculation of the skin friction coefficient of horizontal wavy plates
                        • Author:
                        • Publisher: ➤  von Karman Institute for Fluid Dynamics
                        • Publish Date:
                        • Publish Location: Rhode Saint Genese, Belgium

                        “A method for the approximate calculation of the skin friction coefficient of horizontal wavy plates” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1987
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

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                        15Further developments of the fringe-imaging skin friction technique

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                        “Further developments of the fringe-imaging skin friction technique” Metadata:

                        • Title: ➤  Further developments of the fringe-imaging skin friction technique
                        • Author:
                        • Language: English
                        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
                        • Publish Date:
                        • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                        “Further developments of the fringe-imaging skin friction technique” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1996
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

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                          16Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?

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                          “Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?” Metadata:

                          • Title: ➤  Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?
                          • Author:
                          • Number of Pages: Median: 24
                          • Publisher: AGARD
                          • Publish Date:
                          • Publish Location: Neuilly sur Seine, France

                          “Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?” 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

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                          17Some experimental observations of the law of the wall behind large-eddy breakup devices using servo-controlled skin friction balances

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                          “Some experimental observations of the law of the wall behind large-eddy breakup devices using servo-controlled skin friction balances” Metadata:

                          • Title: ➤  Some experimental observations of the law of the wall behind large-eddy breakup devices using servo-controlled skin friction balances
                          • Author:
                          • Number of Pages: Median: 13
                          • Publisher: AIAA
                          • Publish Date:
                          • Publish Location: Washington, D. C

                          “Some experimental observations of the law of the wall behind large-eddy breakup devices using servo-controlled skin friction balances” 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

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                          18A proof of concept experiment for reducing skin friction by using a micro-blowing technique

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                          “A proof of concept experiment for reducing skin friction by using a micro-blowing technique” Metadata:

                          • Title: ➤  A proof of concept experiment for reducing skin friction by using a micro-blowing technique
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                          • Publish Date:
                          • Publish Location: ➤  Springfield, Va - [Washington, D.C

                          “A proof of concept experiment for reducing skin friction by using a micro-blowing technique” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1996
                          • 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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                            19Computational study of surface tension and wall adhesion effects on an oil film flow underneath an air boundary layer

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                            “Computational study of surface tension and wall adhesion effects on an oil film flow underneath an air boundary layer” Metadata:

                            • Title: ➤  Computational study of surface tension and wall adhesion effects on an oil film flow underneath an air boundary layer
                            • Author:
                            • Language: English
                            • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
                            • Publish Date:
                            • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                            “Computational study of surface tension and wall adhesion effects on an oil film flow underneath an air boundary layer” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1998
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

                            Online Access

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                              20Skin friction determination by LDV measurements in a viscous sublayer - analysis of systematic errors

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                              “Skin friction determination by LDV measurements in a viscous sublayer - analysis of systematic errors” Metadata:

                              • Title: ➤  Skin friction determination by LDV measurements in a viscous sublayer - analysis of systematic errors
                              • Author:
                              • Number of Pages: Median: 83
                              • Publisher: ➤  von Karman Institute for Fluid Dynamics
                              • Publish Date:
                              • Publish Location: Rhode Saint Genese, Belgium

                              “Skin friction determination by LDV measurements in a viscous sublayer - analysis of systematic errors” 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

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                              21Dual cylindrical wave laser-Doppler method for measurement of skin friction in fluid flow

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                              “Dual cylindrical wave laser-Doppler method for measurement of skin friction in fluid flow” Metadata:

                              • Title: ➤  Dual cylindrical wave laser-Doppler method for measurement of skin friction in fluid flow
                              • Author:
                              • Number of Pages: Median: 261
                              • Publisher: Stanford University
                              • Publish Date:
                              • Publish Location: Stanford, Calif

                              “Dual cylindrical wave laser-Doppler method for measurement of skin friction in fluid flow” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

                              • First Year Published: 1987
                              • Is Full Text Available: No
                              • Is The Book Public: No
                              • Access Status: No_ebook

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