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Source: The Open Library

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1Numerical solutions of the complete Navier-Stokes equations

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“Numerical solutions of the complete Navier-Stokes equations” Metadata:

  • Title: ➤  Numerical solutions of the complete Navier-Stokes equations
  • Author:
  • Language: English
  • Publisher: ➤  Dept. of Mechanical and Aerospace Engineering, North Carolina State University - National Aeronautics and Space Administration - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Washington, DC - [Washington, D.C - Raleigh, N.C - Springfield, Va

“Numerical solutions of the complete Navier-Stokes equations” 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

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    2Navier-Stokes simulation of the supersonic combustion flowfield in a ram accelerator

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    “Navier-Stokes simulation of the supersonic combustion flowfield in a ram accelerator” Metadata:

    • Title: ➤  Navier-Stokes simulation of the supersonic combustion flowfield in a ram accelerator
    • Author:
    • Language: English
    • Number of Pages: Median: 23
    • Publisher: ➤  American Institute for Aeronautics and Astronautics - National Aeronautics and Space Administration - For sale by the National Technical Information Service
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - Washington, D. C - [Washington, DC]

    “Navier-Stokes simulation of the supersonic combustion flowfield in a ram accelerator” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1991
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Access

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      3Fuel-rich catalytic combustion of a high density fuel

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      “Fuel-rich catalytic combustion of a high density fuel” Metadata:

      • Title: ➤  Fuel-rich catalytic combustion of a high density fuel
      • Author:
      • Language: English
      • Number of Pages: Median: 11
      • Publisher: ➤  For sale by the National Technical Information Service - Lewis Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
      • Publish Date:
      • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va - Cleveland, Ohio

      “Fuel-rich catalytic combustion of a high density fuel” 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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        4Instrumentation 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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          5Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program

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          “Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program” Metadata:

          • Title: ➤  Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  Edwards, Calif - Springfield, VA

          “Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program” 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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            6Effect of heat release on the spatial stability of a supersonic reacting mixing layer

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            “Effect of heat release on the spatial stability of a supersonic reacting mixing layer” Metadata:

            • Title: ➤  Effect of heat release on the spatial stability of a supersonic reacting mixing layer
            • Author:
            • Number of Pages: Median: 10
            • Publisher: ICASE
            • Publish Date:
            • Publish Location: Hampton, Va

            “Effect of heat release on the spatial stability of a supersonic reacting mixing layer” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1988
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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            7The aerospace plane design challenge

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            “The aerospace plane design challenge” Metadata:

            • Title: ➤  The aerospace plane design challenge
            • Author:
            • Language: English
            • Publisher: NASA Ames Resarch Center
            • Publish Date:
            • Publish Location: Moffett Field, Calif

            “The aerospace plane design challenge” 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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              8Diagnostics in supersonic combustion

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              “Diagnostics in supersonic combustion” Metadata:

              • Title: ➤  Diagnostics in supersonic combustion
              • Author:
              • Publisher: AIAA
              • Publish Date:
              • Publish Location: New York

              “Diagnostics in supersonic combustion” 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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              9Laser-initiated conical detonation wave for supersonic combustion

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              “Laser-initiated conical detonation wave for supersonic combustion” Metadata:

              • Title: ➤  Laser-initiated conical detonation wave for supersonic combustion
              • Author:
              • Number of Pages: Median: 11
              • Publisher: AIAA
              • Publish Date:
              • Publish Location: New York

              “Laser-initiated conical detonation wave for supersonic combustion” 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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              10Analytical and experimental study of supersonic combustion of hydrogen in a vitiated airstream

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              “Analytical and experimental study of supersonic combustion of hydrogen in a vitiated airstream” Metadata:

              • Title: ➤  Analytical and experimental study of supersonic combustion of hydrogen in a vitiated airstream
              • Author:
              • Number of Pages: Median: 25
              • Publisher: Sine nomine
              • Publish Date:
              • Publish Location: [S.l.]

              “Analytical and experimental study of supersonic combustion of hydrogen in a vitiated airstream” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1973
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

              Online Access

              Downloads Are Not Available:

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                11Annual technical report on turbulent reacting flows and supersonic combustion

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                “Annual technical report on turbulent reacting flows and supersonic combustion” Metadata:

                • Title: ➤  Annual technical report on turbulent reacting flows and supersonic combustion
                • Author:
                • Number of Pages: Median: 24
                • Publisher: ➤  Stanford University, High Temperature Gasdynamics Laboratory
                • Publish Date:
                • Publish Location: Stanford, Calif

                “Annual technical report on turbulent reacting flows and supersonic combustion” 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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                12A laser-induced-fluorescence visualization study of transverse, sonic fuel injection in a nonreacting supersonic combustor

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                “A laser-induced-fluorescence visualization study of transverse, sonic fuel injection in a nonreacting supersonic combustor” Metadata:

                • Title: ➤  A laser-induced-fluorescence visualization study of transverse, sonic fuel injection in a nonreacting supersonic combustor
                • Author:
                • Publisher: AIAA
                • Publish Date:
                • Publish Location: New York

                “A laser-induced-fluorescence visualization study of transverse, sonic fuel injection in a nonreacting supersonic combustor” 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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                Find A laser-induced-fluorescence visualization study of transverse, sonic fuel injection in a nonreacting supersonic combustor at online marketplaces:


                13Supersonic mixing and combustion of a hydrogen jet in a coaxial high-temperature test gas

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                “Supersonic mixing and combustion of a hydrogen jet in a coaxial high-temperature test gas” Metadata:

                • Title: ➤  Supersonic mixing and combustion of a hydrogen jet in a coaxial high-temperature test gas
                • Author:
                • Number of Pages: Median: 10
                • Publisher: ➤  American Institute of Aeronautics and Astronautics
                • Publish Date:
                • Publish Location: New York

                “Supersonic mixing and combustion of a hydrogen jet in a coaxial high-temperature test gas” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1972
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

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                14Analysis of losses in supersonic mixing and reacting flows

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                “Analysis of losses in supersonic mixing and reacting flows” Metadata:

                • Title: ➤  Analysis of losses in supersonic mixing and reacting flows
                • Author:
                • Number of Pages: Median: 20
                • Publisher: ➤  American Institute of Aeronautics and Astronautics
                • Publish Date:
                • Publish Location: Washington, D. C

                “Analysis of losses in supersonic mixing and reacting flows” 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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                15A comparative study of scramjet injection strategies for high Mach number flows

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                “A comparative study of scramjet injection strategies for high Mach number flows” Metadata:

                • Title: ➤  A comparative study of scramjet injection strategies for high Mach number flows
                • Author:
                • Number of Pages: Median: 23
                • Publisher: ➤  American Institute of Aeronautics and Astronautics
                • Publish Date:
                • Publish Location: Washington, D. C

                “A comparative study of scramjet injection strategies for high Mach number flows” 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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                16A numerical study of mixing enhancement in a supersonic combustor

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                “A numerical study of mixing enhancement in a supersonic combustor” Metadata:

                • Title: ➤  A numerical study of mixing enhancement in a supersonic combustor
                • Author:
                • Number of Pages: Median: 16
                • Publisher: ➤  American Institute of Aeronautics and Astronautics
                • Publish Date:
                • Publish Location: Washington, D. C

                “A numerical study of mixing enhancement in a supersonic combustor” 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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                17Heat release effects on mixing in supersonic reacting free shear-layers

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                “Heat release effects on mixing in supersonic reacting free shear-layers” Metadata:

                • Title: ➤  Heat release effects on mixing in supersonic reacting free shear-layers
                • Author:
                • Number of Pages: Median: 11
                • Publisher: ➤  American Institute of Aeronautics and Astronautics
                • Publish Date:
                • Publish Location: Washington, D. C

                “Heat release effects on mixing in supersonic reacting free shear-layers” 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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                18Noncircular jet dynamics in supersonic combustion

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                “Noncircular jet dynamics in supersonic combustion” Metadata:

                • Title: ➤  Noncircular jet dynamics in supersonic combustion
                • Author:
                • Publisher: ➤  American Institute of Aeronautics and Astronautics
                • Publish Date:
                • Publish Location: New York

                “Noncircular jet dynamics in supersonic combustion” 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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                19Effect of density gradients in confined supersonic shear layers

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                “Effect of density gradients in confined supersonic shear layers” Metadata:

                • Title: ➤  Effect of density gradients in confined supersonic shear layers
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                • Publish Date:
                • Publish Location: ➤  [Washington, DC - Springfield, Va

                “Effect of density gradients in confined supersonic shear layers” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

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

                Online Access

                Downloads Are Not Available:

                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                  20Supersonic combustion of hydrogen injected perpendicular to a ducted vitiated airstream

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                  “Supersonic combustion of hydrogen injected perpendicular to a ducted vitiated airstream” Metadata:

                  • Title: ➤  Supersonic combustion of hydrogen injected perpendicular to a ducted vitiated airstream
                  • Author:
                  • Number of Pages: Median: 10
                  • Publisher: AIAA
                  • Publish Date:
                  • Publish Location: New York

                  “Supersonic combustion of hydrogen injected perpendicular to a ducted vitiated airstream” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1973
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

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                  21Mixing enhancement in a supersonic combustor

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                  “Mixing enhancement in a supersonic combustor” Metadata:

                  • Title: ➤  Mixing enhancement in a supersonic combustor
                  • Author:
                  • Number of Pages: Median: 15
                  • Publisher: ➤  American Institute of Aeronautics and Astronautics
                  • Publish Date:
                  • Publish Location: Washington, D. C

                  “Mixing enhancement in a supersonic combustor” 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

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                  22Supersonic reacting internal flow fields

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                  “Supersonic reacting internal flow fields” Metadata:

                  • Title: ➤  Supersonic reacting internal flow fields
                  • Author:
                  • Language: English
                  • Number of Pages: Median: 64
                  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                  • Publish Date:
                  • Publish Location: ➤  Springfield, Va - [Washington, D.C.?

                  “Supersonic reacting internal flow fields” 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:

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                    23Vorticity generation by contoured wall injectors

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                    “Vorticity generation by contoured wall injectors” Metadata:

                    • Title: ➤  Vorticity generation by contoured wall injectors
                    • Author:
                    • Number of Pages: Median: 16
                    • Publisher: ➤  American Institute of Aeronautics and Astronautics
                    • Publish Date:
                    • Publish Location: Washington, D. C

                    “Vorticity generation by contoured wall injectors” 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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                    24A two-dimensional numerical simulation of shock-enhanced mixing in a rectangular scramjet flowfield with parallel hydrogen injection

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                    “A two-dimensional numerical simulation of shock-enhanced mixing in a rectangular scramjet flowfield with parallel hydrogen injection” Metadata:

                    • Title: ➤  A two-dimensional numerical simulation of shock-enhanced mixing in a rectangular scramjet flowfield with parallel hydrogen injection
                    • Author:
                    • Number of Pages: Median: 11
                    • Publisher: ➤  American Institute of Aeronautics and Astronautics
                    • Publish Date:
                    • Publish Location: Washington, D. C

                    “A two-dimensional numerical simulation of shock-enhanced mixing in a rectangular scramjet flowfield with parallel hydrogen injection” 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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                    25Evaluation of parallel injector configurations for supersonic combustion

                    By

                    “Evaluation of parallel injector configurations for supersonic combustion” Metadata:

                    • Title: ➤  Evaluation of parallel injector configurations for supersonic combustion
                    • Author:
                    • Number of Pages: Median: 14
                    • Publisher: ➤  American Institute of Aeronautics and Astronautics
                    • Publish Date:
                    • Publish Location: Washington, D. C

                    “Evaluation of parallel injector configurations for supersonic combustion” 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

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                    26A review of supersonic combustion research at AEDC with hypersonic applications

                    By

                    “A review of supersonic combustion research at AEDC with hypersonic applications” Metadata:

                    • Title: ➤  A review of supersonic combustion research at AEDC with hypersonic applications
                    • Author:
                    • Number of Pages: Median: 11
                    • Publisher: ➤  American Institute of Aeronautics and Astronautics
                    • Publish Date:
                    • Publish Location: Washington, D. C

                    “A review of supersonic combustion research at AEDC with hypersonic applications” 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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                    27Planar Rayleigh scattering and laser-induced fluorescence for visualization of a hot, Mach 2 annular air jet

                    By

                    “Planar Rayleigh scattering and laser-induced fluorescence for visualization of a hot, Mach 2 annular air jet” Metadata:

                    • Title: ➤  Planar Rayleigh scattering and laser-induced fluorescence for visualization of a hot, Mach 2 annular air jet
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
                    • Publish Date:
                    • Publish Location: Hampton, Va - [Springfield, Va

                    “Planar Rayleigh scattering and laser-induced fluorescence for visualization of a hot, Mach 2 annular air jet” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

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

                    Online Access

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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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                      28Ignition delays, heats of combustion, and reaction rates of aluminum alkyl derivatives used as ignition and combustion enhancers for supersonic combustion

                      By

                      “Ignition delays, heats of combustion, and reaction rates of aluminum alkyl derivatives used as ignition and combustion enhancers for supersonic combustion” Metadata:

                      • Title: ➤  Ignition delays, heats of combustion, and reaction rates of aluminum alkyl derivatives used as ignition and combustion enhancers for supersonic combustion
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
                      • Publish Date:
                      • Publish Location: ➤  Hampton, Va - [Springfield, Va.?

                      “Ignition delays, heats of combustion, and reaction rates of aluminum alkyl derivatives used as ignition and combustion enhancers for supersonic combustion” 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

                      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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                        29Mixing and combustion enhancement from unsteady shock-fuel layer interactions

                        By

                        “Mixing and combustion enhancement from unsteady shock-fuel layer interactions” Metadata:

                        • Title: ➤  Mixing and combustion enhancement from unsteady shock-fuel layer interactions
                        • Author:
                        • Publisher: ➤  American Institute of Aeronautics and Astronautics
                        • Publish Date:
                        • Publish Location: Washington, D. C

                        “Mixing and combustion enhancement from unsteady shock-fuel layer interactions” 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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                        30Ignition delay and characteristic reaction length in shock induced supersonic combustion

                        By

                        “Ignition delay and characteristic reaction length in shock induced supersonic combustion” Metadata:

                        • Title: ➤  Ignition delay and characteristic reaction length in shock induced supersonic combustion
                        • Author:
                        • Number of Pages: Median: 10
                        • Publisher: AIAA
                        • Publish Date:
                        • Publish Location: New York

                        “Ignition delay and characteristic reaction length in shock induced supersonic combustion” 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

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                        31An analytical and computational investigation of shock-induced vortical flows with applications to supersonic combustion

                        By

                        “An analytical and computational investigation of shock-induced vortical flows with applications to supersonic combustion” Metadata:

                        • Title: ➤  An analytical and computational investigation of shock-induced vortical flows with applications to supersonic combustion
                        • Author:
                        • Number of Pages: Median: 347
                        • Publisher: ➤  California Institute of Technology
                        • Publish Date:
                        • Publish Location: Pasadena, Calif

                        “An analytical and computational investigation of shock-induced vortical flows with applications to supersonic combustion” 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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                        32Progress toward shock enhancement of supersonic combustion processes

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                        “Progress toward shock enhancement of supersonic combustion processes” Metadata:

                        • Title: ➤  Progress toward shock enhancement of supersonic combustion processes
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                        • Publisher: AIAA
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                        • Publish Location: New York

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

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                        33Preliminary calibration of a generic scramjet combustor

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                        “Preliminary calibration of a generic scramjet combustor” Metadata:

                        • Title: ➤  Preliminary calibration of a generic scramjet combustor
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                        • Number of Pages: Median: 28
                        • Publisher: ➤  Institute for Computer Applications in Science and Engineering
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                        • Publish Location: Hampton, Va

                        “Preliminary calibration of a generic scramjet combustor” Subjects and Themes:

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                        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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