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1Study of lee-side flows over conically cambered delta wings at supersonic speeds

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“Study of lee-side flows over conically cambered delta wings at supersonic speeds” Metadata:

  • Title: ➤  Study of lee-side flows over conically cambered delta wings at supersonic speeds
  • Author:
  • Language: English
  • Publisher: ➤  Langley Research Center - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
  • Publish Date:
  • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, D.C.]

“Study of lee-side flows over conically cambered delta wings at supersonic speeds” 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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    2Transonic Navier-Stokes calculations about a 65⁰ delta wing

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    “Transonic Navier-Stokes calculations about a 65⁰ delta wing” Metadata:

    • Title: ➤  Transonic Navier-Stokes calculations about a 65⁰ delta wing
    • 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

    “Transonic Navier-Stokes calculations about a 65⁰ delta wing” 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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      3Delta wings with shock-free cross flow

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      “Delta wings with shock-free cross flow” Metadata:

      • Title: ➤  Delta wings with shock-free cross flow
      • Author:
      • Language: English
      • Publisher: ➤  institute for Computer Applications in Science and Engineering, NASA Langley Research Center
      • Publish Date:
      • Publish Location: Hampton, Va

      “Delta wings with shock-free cross flow” 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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        4Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform

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        “Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform” Metadata:

        • Title: ➤  Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform
        • Author:
        • Number of Pages: Median: 32
        • Publisher: Langley Research Center
        • Publish Date:
        • Publish Location: Hampton, Va

        “Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform” 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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        5Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel

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        “Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel” Metadata:

        • Title: ➤  Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
        • Publish Date:
        • Publish Location: [Washington, D.C.]

        “Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel” 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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          6Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching

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          “Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching” Metadata:

          • Title: ➤  Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration - Mechanical Engineering Dept., Worcester Polytechnic Institute - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  [Washington, DC - Springfield, Va - Worcester, MA

          “Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching” 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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            7Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis

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            “Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis” Metadata:

            • Title: ➤  Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis
            • Author:
            • Language: English
            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
            • Publish Date:
            • Publish Location: ➤  Springfield, Va - [Washington, D.C

            “Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis” 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

            Online Access

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              8The art of sharp-leading-edged delta wings with blowing

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              “The art of sharp-leading-edged delta wings with blowing” Metadata:

              • Title: ➤  The art of sharp-leading-edged delta wings with blowing
              • Author:
              • Language: English
              • Publisher: ➤  Stanford University, Dept. of Aeronautics and Astronautics - Joint Institute for Aeronautics and Acoustics - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: ➤  Stanford, CA - [Springfield, Va

              “The art of sharp-leading-edged delta wings with blowing” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1985
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

              Online Access

              Downloads Are Not Available:

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                9Detailed flow-field measurements over a 75⁰ swept delta wing

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                “Detailed flow-field measurements over a 75⁰ swept delta wing” Metadata:

                • Title: ➤  Detailed flow-field measurements over a 75⁰ swept delta wing
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - National Technical Information Service, distributor]
                • Publish Date:
                • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                “Detailed flow-field measurements over a 75⁰ swept delta wing” 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

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                  10Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications

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                  “Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications” Metadata:

                  • Title: ➤  Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Aeronautics and Space Administration - Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University - National Technical Information Service, distributor
                  • Publish Date:
                  • Publish Location: ➤  [Washington, DC - Norfolk, Va - Springfield, Va

                  “Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications” 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

                  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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                    11Numerical solutions of Navier-Stokes equations for a Butler wing

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                    “Numerical solutions of Navier-Stokes equations for a Butler wing” Metadata:

                    • Title: ➤  Numerical solutions of Navier-Stokes equations for a Butler wing
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - National Aeronautics and Space Administration, Langley Research Center - Old Dominion University Research Foundation
                    • Publish Date:
                    • Publish Location: ➤  Springfield, Va - Hampton, Va - Norfolk, Va - [Washington, DC

                    “Numerical solutions of Navier-Stokes equations for a Butler wing” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 1985
                    • Is Full Text Available: No
                    • Is The Book Public: No
                    • Access Status: No_ebook

                    Online Access

                    Downloads Are Not Available:

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

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                      12Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings

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                      “Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings” Metadata:

                      • Title: ➤  Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings
                      • Author:
                      • Language: English
                      • Number of Pages: Median: 37
                      • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - Stanford University, Dept. of Aeronautics and Astronautics
                      • Publish Date:
                      • Publish Location: ➤  Stanford, Calif - [Moffett Field, Calif.?]

                      “Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

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

                      Online Access

                      Downloads Are Not Available:

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

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                        13Lee-side flow over delta wings at supersonic speeds

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                        “Lee-side flow over delta wings at supersonic speeds” Metadata:

                        • Title: ➤  Lee-side flow over delta wings at supersonic speeds
                        • Author:
                        • Language: English
                        • 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

                        “Lee-side flow over delta wings at supersonic speeds” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1985
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

                        Online Access

                        Downloads Are Not Available:

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

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                          14An exact theory of supersonic flow around a delta wing

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                          “An exact theory of supersonic flow around a delta wing” Metadata:

                          • Title: ➤  An exact theory of supersonic flow around a delta wing
                          • Author:
                          • Number of Pages: Median: 92
                          • Publisher: ➤  [Institute of Aerophysics] - Institute of Aerophysics
                          • Publish Date:
                          • Publish Location: [Downsview, Ont.]

                          “An exact theory of supersonic flow around a delta wing” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1955
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

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                          15Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations

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                          “Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations” Metadata:

                          • Title: ➤  Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations
                          • Author:
                          • Language: English
                          • 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.]

                          “Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations” 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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                            16Lee-side flow over delta wings at supersonic speeds

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                            “Lee-side flow over delta wings at supersonic speeds” Metadata:

                            • Title: ➤  Lee-side flow over delta wings at supersonic speeds
                            • 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

                            “Lee-side flow over delta wings at supersonic speeds” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1985
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

                            Online Access

                            Downloads Are Not Available:

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

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                              17On the swelling and break down of rolled up vortex sheets in inviscid flows around slender delta wings

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                              “On the swelling and break down of rolled up vortex sheets in inviscid flows around slender delta wings” Metadata:

                              • Title: ➤  On the swelling and break down of rolled up vortex sheets in inviscid flows around slender delta wings
                              • Author:
                              • Number of Pages: Median: 20
                              • Publisher: Sine nomine
                              • Publish Date:
                              • Publish Location: [S.l.]

                              “On the swelling and break down of rolled up vortex sheets in inviscid flows around slender delta wings” 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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                              18Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0

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                              “Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0” Metadata:

                              • Title: ➤  Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
                              • Author:
                              • Language: English
                              • Number of Pages: Median: 144
                              • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
                              • Publish Date:
                              • Publish Location: Washington, D.C

                              “Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0” 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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                              19Theoretical and experimental investigation of vortex breakdown

                              By

                              “Theoretical and experimental investigation of vortex breakdown” Metadata:

                              • Title: ➤  Theoretical and experimental investigation of vortex breakdown
                              • Author:
                              • Language: English
                              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                              • Publish Date:
                              • Publish Location: ➤  [Washington, DC - Springfield, Va

                              “Theoretical and experimental investigation of vortex breakdown” 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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                                20An overview of an experimental demonstration aerotow program

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                                “An overview of an experimental demonstration aerotow program” Metadata:

                                • Title: ➤  An overview of an experimental demonstration aerotow program
                                • Author:
                                • Language: English
                                • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
                                • Publish Date:
                                • Publish Location: ➤  [Springfield, Va - Edwards, Calif

                                “An overview of an experimental demonstration aerotow 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

                                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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                                  21Application of the vortex cloud method to slender, flapped delta wings

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                                  “Application of the vortex cloud method to slender, flapped delta wings” Metadata:

                                  • Title: ➤  Application of the vortex cloud method to slender, flapped delta wings
                                  • Author:
                                  • Number of Pages: Median: 84
                                  • Publisher: ➤  [Stanford University, Dept. of Aeronautics and Acoustics?]
                                  • Publish Date:
                                  • Publish Location: [Stanford, Calif?]

                                  “Application of the vortex cloud method to slender, flapped delta wings” 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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                                  22Theoretical studies on flapped delta wings

                                  By

                                  “Theoretical studies on flapped delta wings” Metadata:

                                  • Title: ➤  Theoretical studies on flapped delta wings
                                  • Author:
                                  • Language: English
                                  • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
                                  • Publish Date:
                                  • Publish Location: ➤  [Moffett Field, Calif.] - [Springfield, Va

                                  “Theoretical studies on flapped delta wings” Subjects and Themes:

                                  Edition Identifiers:

                                  Access and General Info:

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

                                  Online Access

                                  Downloads Are Not Available:

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

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                                    23Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data

                                    By

                                    “Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data” Metadata:

                                    • Title: ➤  Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data
                                    • Author:
                                    • Number of Pages: Median: 64
                                    • Publisher: DFVLR
                                    • Publish Date:
                                    • Publish Location: Koln

                                    “Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data” 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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                                    24The influence of the leading edge geometry on the wave drag for a 65 degree delta wing at low supersonic speed and small angles of attack

                                    By

                                    “The influence of the leading edge geometry on the wave drag for a 65 degree delta wing at low supersonic speed and small angles of attack” Metadata:

                                    • Title: ➤  The influence of the leading edge geometry on the wave drag for a 65 degree delta wing at low supersonic speed and small angles of attack
                                    • Author:
                                    • Number of Pages: Median: 12
                                    • Publisher: ➤  Aeronautical Research Institute of Sweden
                                    • Publish Date:
                                    • Publish Location: Stockholm

                                    “The influence of the leading edge geometry on the wave drag for a 65 degree delta wing at low supersonic speed and small angles of attack” 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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                                    25Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing

                                    By

                                    “Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing” Metadata:

                                    • Title: ➤  Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing
                                    • Author:
                                    • Number of Pages: Median: 16
                                    • Publisher: National Aerospace Laboratory
                                    • Publish Date:
                                    • Publish Location: Tokyo

                                    “Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing” 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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                                    26Experimental studies of a delta wing with leading edge flaps

                                    By

                                    “Experimental studies of a delta wing with leading edge flaps” Metadata:

                                    • Title: ➤  Experimental studies of a delta wing with leading edge flaps
                                    • Author:
                                    • Number of Pages: Median: 35
                                    • Publisher: ➤  Joint Institute for Aeronautics and Acoustics
                                    • Publish Date:
                                    • Publish Location: Stanford, Calif

                                    “Experimental studies of a delta wing with leading edge flaps” 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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                                    27Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle

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                                    “Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle” Metadata:

                                    • Title: ➤  Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle
                                    • 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

                                    “Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle” Subjects and Themes:

                                    Edition Identifiers:

                                    Access and General Info:

                                    • First Year Published: 1996
                                    • Is Full Text Available: No
                                    • Is The Book Public: No
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                                      28Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges

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                                      “Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges” Metadata:

                                      • Title: ➤  Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges
                                      • 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

                                      “Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges” Subjects and Themes:

                                      Edition Identifiers:

                                      Access and General Info:

                                      • First Year Published: 1996
                                      • Is Full Text Available: No
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                                        29Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds

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                                        “Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds” Metadata:

                                        • Title: ➤  Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds
                                        • Author:
                                        • Number of Pages: Median: 238
                                        • Publisher: Langley Research Center
                                        • Publish Date:
                                        • Publish Location: Hampton, Va

                                        “Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds” Subjects and Themes:

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                                        • First Year Published: 1987
                                        • Is Full Text Available: No
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                                        30Natural rolling responses of a delta wing in transonic and subsonic flows

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                                        “Natural rolling responses of a delta wing in transonic and subsonic flows” Metadata:

                                        • Title: ➤  Natural rolling responses of a delta wing in transonic and subsonic flows
                                        • Author:
                                        • Language: English
                                        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Aeronautics and Aeronautics
                                        • Publish Date:
                                        • Publish Location: ➤  [Washington, DC - Reston, Va - [Springfield, Va

                                        “Natural rolling responses of a delta wing in transonic and subsonic flows” Subjects and Themes:

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                                        • First Year Published: 1996
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                                          31Unsteady, transonic flow around delta wings undergoing coupled and natural modes response

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                                          “Unsteady, transonic flow around delta wings undergoing coupled and natural modes response” Metadata:

                                          • Title: ➤  Unsteady, transonic flow around delta wings undergoing coupled and natural modes response
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  National Aeronautics and Space Administration - Old Dominion University - National Technical Information Service, distributor
                                          • Publish Date:
                                          • Publish Location: ➤  Springfield, Va - [Norfolk, VA - Washington, D.C

                                          “Unsteady, transonic flow around delta wings undergoing coupled and natural modes response” Subjects and Themes:

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                                          • First Year Published: 1996
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                                          32Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰

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                                          “Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰” Metadata:

                                          • Title: ➤  Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
                                          • Publish Date:
                                          • Publish Location: Hampton, Va

                                          “Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰” Subjects and Themes:

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                                          Access and General Info:

                                          • First Year Published: 1985
                                          • Is Full Text Available: No
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                                            33The aerodynamics of delta wings of elliptical cross-section with separated flow

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                                            “The aerodynamics of delta wings of elliptical cross-section with separated flow” Metadata:

                                            • Title: ➤  The aerodynamics of delta wings of elliptical cross-section with separated flow
                                            • Author:
                                            • Number of Pages: Median: 53
                                            • Publisher: ➤  Stanford University, Dept. of Aeronautics and Astronautics
                                            • Publish Date:
                                            • Publish Location: Stanford, Calif

                                            “The aerodynamics of delta wings of elliptical cross-section with separated flow” Subjects and Themes:

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                                            • First Year Published: 1985
                                            • Is Full Text Available: No
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                                            34Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0

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                                            “Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0” Metadata:

                                            • Title: ➤  Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
                                            • Author:
                                            • Language: English
                                            • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
                                            • Publish Date:
                                            • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                            “Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0” Subjects and Themes:

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                                            • First Year Published: 1993
                                            • Is Full Text Available: No
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                                              35Effective control of computationally simulated wing rock in subsonic flow

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                                              “Effective control of computationally simulated wing rock in subsonic flow” Metadata:

                                              • Title: ➤  Effective control of computationally simulated wing rock in subsonic flow
                                              • Author:
                                              • Language: English
                                              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                              • Publish Date:
                                              • Publish Location: ➤  [Washington, DC - Springfield, Va

                                              “Effective control of computationally simulated wing rock in subsonic flow” Subjects and Themes:

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                                              • First Year Published: 1997
                                              • Is Full Text Available: No
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                                                36Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wing

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                                                “Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wing” Metadata:

                                                • Title: ➤  Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wing
                                                • Author:
                                                • Number of Pages: Median: 167
                                                • Publisher: Langley Research Center
                                                • Publish Date:
                                                • Publish Location: Hampton, Va

                                                “Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wing” Subjects and Themes:

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                                                • First Year Published: 1992
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                                                37Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations

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                                                “Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations” Metadata:

                                                • Title: ➤  Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations
                                                • 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

                                                “Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations” Subjects and Themes:

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                                                • First Year Published: 1999
                                                • Is Full Text Available: No
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                                                  38Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16

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                                                  “Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16” Metadata:

                                                  • Title: ➤  Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16
                                                  • Author:
                                                  • Language: English
                                                  • 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.]

                                                  “Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16” 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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                                                    39Transonic Navier-Stokes calculations about a 65 degree Delta wing

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                                                    “Transonic Navier-Stokes calculations about a 65 degree Delta wing” Metadata:

                                                    • Title: ➤  Transonic Navier-Stokes calculations about a 65 degree Delta wing
                                                    • Author:
                                                    • Number of Pages: Median: 67
                                                    • Publisher: Langley Research Center
                                                    • Publish Date:
                                                    • Publish Location: Hampton, Va

                                                    “Transonic Navier-Stokes calculations about a 65 degree Delta wing” Subjects and Themes:

                                                    Edition Identifiers:

                                                    Access and General Info:

                                                    • First Year Published: 1994
                                                    • Is Full Text Available: No
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                                                    40Numerical solutions of Navier-Stokes equations for a Butler wing

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                                                    “Numerical solutions of Navier-Stokes equations for a Butler wing” Metadata:

                                                    • Title: ➤  Numerical solutions of Navier-Stokes equations for a Butler wing
                                                    • Author:
                                                    • Number of Pages: Median: 44
                                                    • Publisher: ➤  Dept. of Mechanical Engineering and Mechanics, School of Engineering, Old Dominion University
                                                    • Publish Date:
                                                    • Publish Location: Norfolk, Va

                                                    “Numerical solutions of Navier-Stokes equations for a Butler wing” Subjects and Themes:

                                                    Edition Identifiers:

                                                    Access and General Info:

                                                    • First Year Published: 1985
                                                    • Is Full Text Available: No
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                                                    41Evaluation of LDA 3-component velocity data on a 65 [degree] delta wing at M=0.85 and first results of an analysis

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                                                    “Evaluation of LDA 3-component velocity data on a 65 [degree] delta wing at M=0.85 and first results of an analysis” Metadata:

                                                    • Title: ➤  Evaluation of LDA 3-component velocity data on a 65 [degree] delta wing at M=0.85 and first results of an analysis
                                                    • Author:
                                                    • Number of Pages: Median: 63
                                                    • Publisher: DFVLR
                                                    • Publish Date:
                                                    • Publish Location: Koln

                                                    “Evaluation of LDA 3-component velocity data on a 65 [degree] delta wing at M=0.85 and first results of an analysis” Subjects and Themes:

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                                                    • First Year Published: 1989
                                                    • Is Full Text Available: No
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                                                    42The performance of 60 deg delta wings: the effects of leading edge radius and vortex flaps

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                                                    “The performance of 60 deg delta wings: the effects of leading edge radius and vortex flaps” Metadata:

                                                    • Title: ➤  The performance of 60 deg delta wings: the effects of leading edge radius and vortex flaps
                                                    • Author:
                                                    • Number of Pages: Median: 23
                                                    • Publisher: ➤  College of Aeronautics, Cranfield Institute of Technology
                                                    • Publish Date:
                                                    • Publish Location: Cranfield, Bedford

                                                    “The performance of 60 deg delta wings: the effects of leading edge radius and vortex flaps” Subjects and Themes:

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                                                    • First Year Published: 1989
                                                    • Is Full Text Available: No
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                                                    43The performance of 60 degree delta wings: the effects of leading edge radius on vortex flaps and the wing

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                                                    “The performance of 60 degree delta wings: the effects of leading edge radius on vortex flaps and the wing” Metadata:

                                                    • Title: ➤  The performance of 60 degree delta wings: the effects of leading edge radius on vortex flaps and the wing
                                                    • Author:
                                                    • Number of Pages: Median: 34
                                                    • Publisher: ➤  Cranfield Institute of Technology, College of Aeronautics
                                                    • Publish Date:
                                                    • Publish Location: Cranfield, Bedford

                                                    “The performance of 60 degree delta wings: the effects of leading edge radius on vortex flaps and the wing” Subjects and Themes:

                                                    Edition Identifiers:

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                                                    • First Year Published: 1990
                                                    • Is Full Text Available: No
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                                                    44Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges

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                                                    “Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges” Metadata:

                                                    • Title: ➤  Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges
                                                    • Author:
                                                    • Number of Pages: Median: 19
                                                    • Publisher: AIAA
                                                    • Publish Date:
                                                    • Publish Location: New York

                                                    “Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges” Subjects and Themes:

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                                                    • First Year Published: 1978
                                                    • Is Full Text Available: No
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                                                    45A visualisation study of the vortex flow around double-delta wings

                                                    By

                                                    “A visualisation study of the vortex flow around double-delta wings” Metadata:

                                                    • Title: ➤  A visualisation study of the vortex flow around double-delta wings
                                                    • Author:
                                                    • Number of Pages: Median: 12
                                                    • Publisher: ➤  Aeronautical Research Laboratories
                                                    • Publish Date:
                                                    • Publish Location: Melbourne, Vic

                                                    “A visualisation study of the vortex flow around double-delta wings” Subjects and Themes:

                                                    Edition Identifiers:

                                                    Access and General Info:

                                                    • First Year Published: 1985
                                                    • Is Full Text Available: No
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                                                    46An analysis of conical augmentor/delta wing integration

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                                                    “An analysis of conical augmentor/delta wing integration” Metadata:

                                                    • Title: ➤  An analysis of conical augmentor/delta wing integration
                                                    • Author:
                                                    • Number of Pages: Median: 22
                                                    • Publisher: ➤  Stanford University, Department of Aeronautics and Astronautics
                                                    • Publish Date:
                                                    • Publish Location: Stanford, Calif

                                                    “An analysis of conical augmentor/delta wing integration” Subjects and Themes:

                                                    Edition Identifiers:

                                                    Access and General Info:

                                                    • First Year Published: 1987
                                                    • Is Full Text Available: No
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                                                    47The lift of sharp-leading-edged delta wings with blowing

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                                                    “The lift of sharp-leading-edged delta wings with blowing” Metadata:

                                                    • Title: ➤  The lift of sharp-leading-edged delta wings with blowing
                                                    • Author:
                                                    • Number of Pages: Median: 17
                                                    • Publisher: ➤  Stanford University, Dept. of Aeronautics and Astronautics
                                                    • Publish Date:
                                                    • Publish Location: Stanford, Calif

                                                    “The lift of sharp-leading-edged delta wings with blowing” Subjects and Themes:

                                                    Edition Identifiers:

                                                    Access and General Info:

                                                    • First Year Published: 1985
                                                    • Is Full Text Available: No
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                                                    48Numerical solution of flow fields around delta wings using Euler equation methods. Pt. II. Analysis of the results and comparison with experiments

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                                                    “Numerical solution of flow fields around delta wings using Euler equation methods. Pt. II. Analysis of the results and comparison with experiments” Metadata:

                                                    • Title: ➤  Numerical solution of flow fields around delta wings using Euler equation methods. Pt. II. Analysis of the results and comparison with experiments
                                                    • Author:
                                                    • Number of Pages: Median: 24
                                                    • Publisher: DFVLR
                                                    • Publish Date:
                                                    • Publish Location: Braunschweig

                                                    “Numerical solution of flow fields around delta wings using Euler equation methods. Pt. II. Analysis of the results and comparison with experiments” 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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