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1Dual methods and approximation concepts in structural synthesis

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“Dual methods and approximation concepts in structural synthesis” Metadata:

  • Title: ➤  Dual methods and approximation concepts in structural synthesis
  • Author:
  • Language: English
  • Number of Pages: Median: 210
  • 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

“Dual methods and approximation concepts in structural synthesis” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1980
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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2The Delta Wing

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“The Delta Wing” Metadata:

  • Title: The Delta Wing
  • Author:
  • Language: English
  • Number of Pages: Median: 126
  • Publisher: ➤  Iowa State University Press - Iowa State Press
  • Publish Date:
  • Publish Location: Ames

“The Delta Wing” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1981
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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    3The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps

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    “The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps” Metadata:

    • Title: ➤  The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
    • Publish Date:
    • Publish Location: [Washington, D.C.?]

    “The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1984
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Access

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      4High-alpha vortex decoupling investigations on a chine forebody/delta wing configuration at transonic mach numbers

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      “High-alpha vortex decoupling investigations on a chine forebody/delta wing configuration at transonic mach numbers” Metadata:

      • Title: ➤  High-alpha vortex decoupling investigations on a chine forebody/delta wing configuration at transonic mach numbers
      • 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

      “High-alpha vortex decoupling investigations on a chine forebody/delta wing configuration at transonic mach numbers” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

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

      Online Access

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        5Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings

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        “Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings” Metadata:

        • Title: ➤  Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings
        • Author:
        • Language: English
        • Number of Pages: Median: 99
        • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Langley Research Center - For sale by the National Technical Information Service]
        • Publish Date:
        • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, DC]

        “Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings” 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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          6Evaluation of Navier-Stokes and Euler solutions for leading-edge separation vortices

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          “Evaluation of Navier-Stokes and Euler solutions for leading-edge separation vortices” Metadata:

          • Title: ➤  Evaluation of Navier-Stokes and Euler solutions for leading-edge separation vortices
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service
          • Publish Date:
          • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

          “Evaluation of Navier-Stokes and Euler solutions for leading-edge separation vortices” 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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            7Some low-speed flutter characteristics of simple low-aspect-ration delta wing models

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            “Some low-speed flutter characteristics of simple low-aspect-ration delta wing models” Metadata:

            • Title: ➤  Some low-speed flutter characteristics of simple low-aspect-ration delta wing models
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
            • Publish Date:
            • Publish Location: Hampton, Va

            “Some low-speed flutter characteristics of simple low-aspect-ration delta wing models” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1989
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

            Online Access

            Downloads Are Not Available:

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

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              8The natural flow wing-design concept

              By

              “The natural flow wing-design concept” Metadata:

              • Title: ➤  The natural flow wing-design concept
              • Author:
              • Language: English
              • Number of Pages: Median: 40
              • Publisher: ➤  Langley Research Center - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
              • Publish Date:
              • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, DC]

              “The natural flow wing-design concept” 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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                9Uniform approximation to the shock generated by thin, nonlifting wings of rectangular planform

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                “Uniform approximation to the shock generated by thin, nonlifting wings of rectangular planform” Metadata:

                • Title: ➤  Uniform approximation to the shock generated by thin, nonlifting wings of rectangular planform
                • Author:
                • Language: English
                • Number of Pages: Median: 77
                • Publish Date:
                • Publish Location: [New York?] - New York]

                “Uniform approximation to the shock generated by thin, nonlifting wings of rectangular planform” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1969
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

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                10Delta wings with shock-free cross flow

                By

                “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

                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 simulation of a powered-lift landing, tracking flow features using overset grids, and simulation of high lift devices on a fighter-lift-and-control wing

                  By

                  “Numerical simulation of a powered-lift landing, tracking flow features using overset grids, and simulation of high lift devices on a fighter-lift-and-control wing” Metadata:

                  • Title: ➤  Numerical simulation of a powered-lift landing, tracking flow features using overset grids, and simulation of high lift devices on a fighter-lift-and-control wing
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Aeronautics and Space Administration - MCAT Institute - National Technical Information Service, distributor
                  • Publish Date:
                  • Publish Location: ➤  Springfield, Va - San Jose, CA - [Washington, DC

                  “Numerical simulation of a powered-lift landing, tracking flow features using overset grids, and simulation of high lift devices on a fighter-lift-and-control wing” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

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

                  Online Access

                  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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                    12Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2

                    By

                    “Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2” Metadata:

                    • Title: ➤  Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2
                    • Author:
                    • Language: English
                    • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
                    • Publish Date:
                    • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                    “Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2” 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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                      13The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps

                      By

                      “The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps” Metadata:

                      • Title: ➤  The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
                      • Publish Date:
                      • Publish Location: [Washington, D.C.?]

                      “The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

                      • First Year Published: 1984
                      • Is Full Text Available: No
                      • Is The Book Public: No
                      • Access Status: No_ebook

                      Online Access

                      Downloads Are Not Available:

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

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                        14Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations

                        By

                        “Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations” Metadata:

                        • Title: ➤  Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 37
                        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Service - for sale by the National Technical Information Service
                        • Publish Date:
                        • Publish Location: Springfield, Va - [Washington]

                        “Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations” 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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                        15Experimental and theoretical study of three interacting, closely-spaced, sharp-edged 60⁰

                        By

                        “Experimental and theoretical study of three interacting, closely-spaced, sharp-edged 60⁰” Metadata:

                        • Title: ➤  Experimental and theoretical study of three interacting, closely-spaced, sharp-edged 60⁰
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 44
                        • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
                        • Publish Date:
                        • Publish Location: ➤  Washington, D.C - [Springfield, Va

                        “Experimental and theoretical study of three interacting, closely-spaced, sharp-edged 60⁰” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1981
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

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                        16Development of aerodynamic prediction methods for irregular planform wings

                        By

                        “Development of aerodynamic prediction methods for irregular planform wings” Metadata:

                        • Title: ➤  Development of aerodynamic prediction methods for irregular planform wings
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 442
                        • 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

                        “Development of aerodynamic prediction methods for irregular planform wings” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

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

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                        17Numerical solutions of Navier-Stokes equations for a Butler wing

                        By

                        “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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                          18Tests at subsonic and supersonic speeds on a slender cambered wing with fin, underwing engine nacelles and trailing-edge controls

                          By

                          “Tests at subsonic and supersonic speeds on a slender cambered wing with fin, underwing engine nacelles and trailing-edge controls” Metadata:

                          • Title: ➤  Tests at subsonic and supersonic speeds on a slender cambered wing with fin, underwing engine nacelles and trailing-edge controls
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 57
                          • Publisher: ➤  H.M.S.O. - Stationery Office, The
                          • Publish Date:
                          • Publish Location: London

                          “Tests at subsonic and supersonic speeds on a slender cambered wing with fin, underwing engine nacelles and trailing-edge controls” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1969
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

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                          19Low-speed characteristics of waverider wings

                          By

                          “Low-speed characteristics of waverider wings” Metadata:

                          • Title: ➤  Low-speed characteristics of waverider wings
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 21
                          • Publisher: H.M. Stationery Off.
                          • Publish Date:
                          • Publish Location: London

                          “Low-speed characteristics of waverider wings” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

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

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                          20The pressure distribution at zero lift on a slender delta wing at transonic speeds

                          By

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

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

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

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1968
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

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                          21Further measurements of transient pressures on a narrow-delta wing due to a vertical gust

                          By

                          “Further measurements of transient pressures on a narrow-delta wing due to a vertical gust” Metadata:

                          • Title: ➤  Further measurements of transient pressures on a narrow-delta wing due to a vertical gust
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 14
                          • Publisher: H.M.S.O.
                          • Publish Date:
                          • Publish Location: London

                          “Further measurements of transient pressures on a narrow-delta wing due to a vertical gust” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1968
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

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                          22An experimental study of the hypersonic flow about a particular half-cone-and-delta-wing lifting configuration

                          By

                          “An experimental study of the hypersonic flow about a particular half-cone-and-delta-wing lifting configuration” Metadata:

                          • Title: ➤  An experimental study of the hypersonic flow about a particular half-cone-and-delta-wing lifting configuration
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Research Council of Canada
                          • Publish Date:
                          • Publish Location: Ottawa

                          “An experimental study of the hypersonic flow about a particular half-cone-and-delta-wing lifting configuration” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

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

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                          23Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds

                          By

                          “Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds” Metadata:

                          • Title: ➤  Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 11
                          • Publisher: H.M.S.O.
                          • Publish Date:
                          • Publish Location: London

                          “Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

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

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                          24Supersonic flutter derivatives for a series of swept and cropped delta wings

                          By

                          “Supersonic flutter derivatives for a series of swept and cropped delta wings” Metadata:

                          • Title: ➤  Supersonic flutter derivatives for a series of swept and cropped delta wings
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 18
                          • Publisher: H.M.S.O.
                          • Publish Date:
                          • Publish Location: London

                          “Supersonic flutter derivatives for a series of swept and cropped delta wings” Subjects and Themes:

                          Edition Identifiers:

                          • The Open Library ID: OL5574903M
                          • Online Computer Library Center (OCLC) ID: 6163296
                          • Library of Congress Control Number (LCCN): 67085727

                          Access and General Info:

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

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                          25Low-speed wind-tunnel measurements of the lift, drag and pitching moment on three symmetrical ogee-wing models and on a symmetrical slender wing-body model

                          By

                          “Low-speed wind-tunnel measurements of the lift, drag and pitching moment on three symmetrical ogee-wing models and on a symmetrical slender wing-body model” Metadata:

                          • Title: ➤  Low-speed wind-tunnel measurements of the lift, drag and pitching moment on three symmetrical ogee-wing models and on a symmetrical slender wing-body model
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 25
                          • Publisher: H.M.S.O.
                          • Publish Date:
                          • Publish Location: London

                          “Low-speed wind-tunnel measurements of the lift, drag and pitching moment on three symmetrical ogee-wing models and on a symmetrical slender wing-body model” Subjects and Themes:

                          Edition Identifiers:

                          • The Open Library ID: OL5568464M
                          • Online Computer Library Center (OCLC) ID: 6157601
                          • Library of Congress Control Number (LCCN): 67075153

                          Access and General Info:

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

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                          Find Low-speed wind-tunnel measurements of the lift, drag and pitching moment on three symmetrical ogee-wing models and on a symmetrical slender wing-body model at online marketplaces:


                          26Exploratory investigation of the effects of blowing from the leading edge of a delta wing

                          By

                          “Exploratory investigation of the effects of blowing from the leading edge of a delta wing” Metadata:

                          • Title: ➤  Exploratory investigation of the effects of blowing from the leading edge of a delta wing
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 19
                          • Publisher: H.M.S.O.
                          • Publish Date:
                          • Publish Location: London

                          “Exploratory investigation of the effects of blowing from the leading edge of a delta wing” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1968
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

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                          27Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results

                          By

                          “Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results” Metadata:

                          • Title: ➤  Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 57
                          • Publisher: H.M.S.O.
                          • Publish Date:
                          • Publish Location: London

                          “Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results” Subjects and Themes:

                          Edition Identifiers:

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                          • First Year Published: 1969
                          • Is Full Text Available: No
                          • Is The Book Public: No
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                          28The separated flows on slender wings in unsteady motion

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                          “The separated flows on slender wings in unsteady motion” Metadata:

                          • Title: ➤  The separated flows on slender wings in unsteady motion
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 36
                          • Publisher: H.M.S.O.
                          • Publish Date:
                          • Publish Location: London

                          “The separated flows on slender wings in unsteady motion” Subjects and Themes:

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                          • First Year Published: 1967
                          • Is Full Text Available: No
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                          29Pressure distributions on planar and cruciform delta wings attached to cylindrical bodies in supersonic flow

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                          “Pressure distributions on planar and cruciform delta wings attached to cylindrical bodies in supersonic flow” Metadata:

                          • Title: ➤  Pressure distributions on planar and cruciform delta wings attached to cylindrical bodies in supersonic flow
                          • Author:
                          • Language: English
                          • Publisher: ➤  Dept. of Supply, Australian Aeronautical Research Committee
                          • Publish Date:
                          • Publish Location: [Melbourne]

                          “Pressure distributions on planar and cruciform delta wings attached to cylindrical bodies in supersonic flow” Subjects and Themes:

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                          • First Year Published: 1900
                          • Is Full Text Available: No
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                          30Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177) with blowing over the trailing-edge flaps and ailerons

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                          “Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177) with blowing over the trailing-edge flaps and ailerons” Metadata:

                          • Title: ➤  Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177) with blowing over the trailing-edge flaps and ailerons
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 32
                          • Publisher: H.M.S.O.
                          • Publish Date:
                          • Publish Location: London

                          “Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177) with blowing over the trailing-edge flaps and ailerons” Subjects and Themes:

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                          • First Year Published: 1966
                          • Is Full Text Available: No
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                          31Evaluation of LDA 3-component velocity data on a 65 ̊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 ̊delta wing at M=0.85 and first results of an analysis” Metadata:

                          • Title: ➤  Evaluation of LDA 3-component velocity data on a 65 ̊delta wing at M=0.85 and first results of an analysis
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 63
                          • Publish Date:
                          • Publish Location: ➤  Göttingen : DFVLR, Institut für Experimentelle Strömungsmechanik

                          “Evaluation of LDA 3-component velocity data on a 65 ̊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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                          32Transonic and supersonic flow past a 65⁰ delta wing with rounded leading edges

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                          “Transonic and supersonic flow past a 65⁰ delta wing with rounded leading edges” Metadata:

                          • Title: ➤  Transonic and supersonic flow past a 65⁰ delta wing with rounded leading edges
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 64
                          • Publisher: ➤  DFVLR, Institut für Experimentelle Strömungsmechanik
                          • Publish Date:
                          • Publish Location: Göttingen

                          “Transonic and supersonic flow past a 65⁰ delta wing with rounded leading edges” Subjects and Themes:

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                          • First Year Published: 1988
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                          33Proceedings of 1st International Hypersonic Waverider Symposium, October 17-19, 1990, University of Maryland, College Park, Maryland, U.S.A

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                          “Proceedings of 1st International Hypersonic Waverider Symposium, October 17-19, 1990, University of Maryland, College Park, Maryland, U.S.A” Metadata:

                          • Title: ➤  Proceedings of 1st International Hypersonic Waverider Symposium, October 17-19, 1990, University of Maryland, College Park, Maryland, U.S.A
                          • Author: ➤  
                          • Language: English
                          • Publisher: The University
                          • Publish Date:
                          • Publish Location: [College Park, Md.]

                          “Proceedings of 1st International Hypersonic Waverider Symposium, October 17-19, 1990, University of Maryland, College Park, Maryland, U.S.A” Subjects and Themes:

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                          • First Year Published: 1990
                          • Is Full Text Available: No
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                          34Treugolʹnye krylʹi͡a︡ v giperzvukovom potoke

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                          “Treugolʹnye krylʹi͡a︡ v giperzvukovom potoke” Metadata:

                          • Title: ➤  Treugolʹnye krylʹi͡a︡ v giperzvukovom potoke
                          • Author:
                          • Language: rus
                          • Number of Pages: Median: 135
                          • Publisher: "Mashinostroenie"
                          • Publish Date:
                          • Publish Location: Moskva

                          “Treugolʹnye krylʹi͡a︡ v giperzvukovom potoke” Subjects and Themes:

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                          • First Year Published: 1984
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

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                          35Aerodynamische Untersuchungen an Doppeldeltaflügeln bei unsymmetrischer Strömung =

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                          “Aerodynamische Untersuchungen an Doppeldeltaflügeln bei unsymmetrischer Strömung =” Metadata:

                          • Title: ➤  Aerodynamische Untersuchungen an Doppeldeltaflügeln bei unsymmetrischer Strömung =
                          • Author:
                          • Language: ger
                          • Number of Pages: Median: 100
                          • Publisher: ➤  Dokumentationszentrum der Bundeswehr
                          • Publish Date:
                          • Publish Location: Bonn

                          “Aerodynamische Untersuchungen an Doppeldeltaflügeln bei unsymmetrischer Strömung =” Subjects and Themes:

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                          • First Year Published: 1987
                          • Is Full Text Available: No
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                          36Investigation of asymmetry of vortex flow over slender delta wings

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                          “Investigation of asymmetry of vortex flow over slender delta wings” Metadata:

                          • Title: ➤  Investigation of asymmetry of vortex flow over slender delta wings
                          • Author:
                          • Language: English
                          • Publish Date:

                          “Investigation of asymmetry of vortex flow over slender delta wings” Subjects and Themes:

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                          • First Year Published: 2011
                          • Is Full Text Available: No
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                          37Vortical solutions of the conical Euler equations

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                          Book's cover

                          “Vortical solutions of the conical Euler equations” Metadata:

                          • Title: ➤  Vortical solutions of the conical Euler equations
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 285
                          • Publisher: Vieweg
                          • Publish Date:
                          • Publish Location: Braunschweig

                          “Vortical solutions of the conical Euler equations” Subjects and Themes:

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                          • First Year Published: 1990
                          • Is Full Text Available: No
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                          38Heat transfer and transition measurements at M=8.5 on a delta model and a flat plate at incidence

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                          “Heat transfer and transition measurements at M=8.5 on a delta model and a flat plate at incidence” Metadata:

                          • Title: ➤  Heat transfer and transition measurements at M=8.5 on a delta model and a flat plate at incidence
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 32
                          • Publisher: H.M.S.O.
                          • Publish Date:
                          • Publish Location: London

                          “Heat transfer and transition measurements at M=8.5 on a delta model and a flat plate at incidence” Subjects and Themes:

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                          Access and General Info:

                          • First Year Published: 1969
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

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                          39Turbulente Strömungsstrukturen an Flugzeugkonfigurationen mit Vorderkantenwirbeln

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                          “Turbulente Strömungsstrukturen an Flugzeugkonfigurationen mit Vorderkantenwirbeln” Metadata:

                          • Title: ➤  Turbulente Strömungsstrukturen an Flugzeugkonfigurationen mit Vorderkantenwirbeln
                          • Author:
                          • Language: ger
                          • Number of Pages: Median: 335
                          • Publisher: Utz, Wissenschaft
                          • Publish Date:
                          • Publish Location: München

                          “Turbulente Strömungsstrukturen an Flugzeugkonfigurationen mit Vorderkantenwirbeln” Subjects and Themes:

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                          • First Year Published: 1997
                          • Is Full Text Available: No
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                          40Static 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:
                          • Language: English
                          • Number of Pages: Median: 32
                          • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
                          • Publish Date:
                          • Publish Location: ➤  [Springfield, Va - Washington, D.C

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

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                          • First Year Published: 1990
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

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                          41Lift augmentation on a delta wing via leading edge fences and the Gurney flap

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                          “Lift augmentation on a delta wing via leading edge fences and the Gurney flap” Metadata:

                          • Title: ➤  Lift augmentation on a delta wing via leading edge fences and the Gurney flap
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                          • Publish Date:
                          • Publish Location: ➤  Springfield, Va - [Washington, DC

                          “Lift augmentation on a delta wing via leading edge fences and the Gurney flap” 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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                            42Numerical study of delta wing leading edge blowing

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                            “Numerical study of delta wing leading edge blowing” Metadata:

                            • Title: ➤  Numerical study of delta wing leading edge blowing
                            • Author:
                            • Language: English
                            • Publisher: ➤  For sale by the National Technical Information Service - Joint Institute for Aeronautics and Acoustics
                            • Publish Date:
                            • Publish Location: ➤  Stanford, CA - [Springfield, Va

                            “Numerical study of delta wing leading edge blowing” Subjects and Themes:

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                            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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                              43Force and moment measurements on a 74ê delta wing with an apex flap (data report)

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                              “Force and moment measurements on a 74ê delta wing with an apex flap (data report)” Metadata:

                              • Title: ➤  Force and moment measurements on a 74ê delta wing with an apex flap (data report)
                              • Author:
                              • Language: English
                              • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
                              • Publish Date:
                              • Publish Location: Hampton, Va

                              “Force and moment measurements on a 74ê delta wing with an apex flap (data report)” 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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                                44Configuration heating for a hypersonic research airplane concept having a 70ê swept double-delta wing

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                                “Configuration heating for a hypersonic research airplane concept having a 70ê swept double-delta wing” Metadata:

                                • Title: ➤  Configuration heating for a hypersonic research airplane concept having a 70ê swept double-delta wing
                                • Author:
                                • Language: English
                                • Number of Pages: Median: 73
                                • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
                                • Publish Date:
                                • Publish Location: [Washington] - Springfield, Va

                                “Configuration heating for a hypersonic research airplane concept having a 70ê swept double-delta wing” Subjects and Themes:

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                                Access and General Info:

                                • First Year Published: 1978
                                • Is Full Text Available: No
                                • Is The Book Public: No
                                • Access Status: No_ebook

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                                45Conical Euler analysis and active roll suppression for unsteady vortical flows about rolling delta wings

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                                “Conical Euler analysis and active roll suppression for unsteady vortical flows about rolling delta wings” Metadata:

                                • Title: ➤  Conical Euler analysis and active roll suppression for unsteady vortical flows about rolling delta wings
                                • Author:
                                • Language: English
                                • Publisher: ➤  National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
                                • Publish Date:
                                • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                “Conical Euler analysis and active roll suppression for unsteady vortical flows about rolling delta wings” Subjects and Themes:

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                                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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                                  46Conical Euler analysis and active roll suppression for unsteady vortical flows about rolling delta wings

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                                  “Conical Euler analysis and active roll suppression for unsteady vortical flows about rolling delta wings” Metadata:

                                  • Title: ➤  Conical Euler analysis and active roll suppression for unsteady vortical flows about rolling delta wings
                                  • Author:
                                  • Language: English
                                  • Publisher: ➤  National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
                                  • Publish Date:
                                  • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                  “Conical Euler analysis and active roll suppression for unsteady vortical flows about rolling delta wings” 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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                                    47Subsonic investigations of vortex interaction control for enhanced high-alpha aerodynamics of a chine forebody/delta wing configuration

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                                    “Subsonic investigations of vortex interaction control for enhanced high-alpha aerodynamics of a chine forebody/delta wing configuration” Metadata:

                                    • Title: ➤  Subsonic investigations of vortex interaction control for enhanced high-alpha aerodynamics of a chine forebody/delta wing configuration
                                    • 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

                                    “Subsonic investigations of vortex interaction control for enhanced high-alpha aerodynamics of a chine forebody/delta wing configuration” Subjects and Themes:

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                                    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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                                      48Development of aerodynamic prediction methods for irregular planform wings

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                                      “Development of aerodynamic prediction methods for irregular planform wings” Metadata:

                                      • Title: ➤  Development of aerodynamic prediction methods for irregular planform wings
                                      • Author:
                                      • Language: English
                                      • Number of Pages: Median: 442
                                      • 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

                                      “Development of aerodynamic prediction methods for irregular planform wings” Subjects and Themes:

                                      Edition Identifiers:

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                                      • First Year Published: 1983
                                      • Is Full Text Available: No
                                      • Is The Book Public: No
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                                      49An aerodynamic model for one and two degree of freedom wing rock of slender delta wings

                                      By

                                      “An aerodynamic model for one and two degree of freedom wing rock of slender delta wings” Metadata:

                                      • Title: ➤  An aerodynamic model for one and two degree of freedom wing rock of slender delta wings
                                      • Author:
                                      • Language: English
                                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
                                      • Publish Date:
                                      • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                                      “An aerodynamic model for one and two degree of freedom wing rock of slender delta wings” 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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                                        50Effects of forebody strakes and Mach number on overall aerodynamic characteristics on configuration with 55ʻ́ cropped delta wing

                                        By

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

                                        • Title: ➤  Effects of forebody strakes and Mach number on overall aerodynamic characteristics on configuration with 55ʻ́ cropped delta wing
                                        • Author:
                                        • Language: English
                                        • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
                                        • Publish Date:
                                        • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                        “Effects of forebody strakes and Mach number on overall aerodynamic characteristics on configuration with 55ʻ́ cropped 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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