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1Shape and flow

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Book's cover

“Shape and flow” Metadata:

  • Title: Shape and flow
  • Author:
  • Language: English
  • Number of Pages: Median: 186
  • Publisher: ➤  Anchor Books - Heinemann - Anchor Books/ Doubleday
  • Publish Date:
  • Publish Location: Garden City, N.Y - London

“Shape and flow” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1961
  • Is Full Text Available: Yes
  • Is The Book Public: No
  • Access Status: Borrowable

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2Theory of satellite orbits in an atmosphere

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Book's cover

“Theory of satellite orbits in an atmosphere” Metadata:

  • Title: ➤  Theory of satellite orbits in an atmosphere
  • Author:
  • Language: English
  • Number of Pages: Median: 165
  • Publisher: Butterworths
  • Publish Date:
  • Publish Location: London

“Theory of satellite orbits in an atmosphere” Subjects and Themes:

Edition Identifiers:

  • The Open Library ID: OL5906431M
  • Online Computer Library Center (OCLC) ID: 2312579
  • Library of Congress Control Number (LCCN): 64005703

Access and General Info:

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

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3Viscous Flow Drag Reduction Paas72 (Progress in astronautics and aeronautics)

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Book's cover

“Viscous Flow Drag Reduction Paas72 (Progress in astronautics and aeronautics)” Metadata:

  • Title: ➤  Viscous Flow Drag Reduction Paas72 (Progress in astronautics and aeronautics)
  • Author:
  • Language: English
  • Number of Pages: Median: 453
  • Publisher: ➤  American Institute of Aeronautics and Astronautics - Amer Inst of Aeronautics &
  • Publish Date:
  • Publish Location: New York

“Viscous Flow Drag Reduction Paas72 (Progress in astronautics and aeronautics)” Subjects and Themes:

Edition Identifiers:

Access and General Info:

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

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4Fluid-dynamic drag

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Book's cover

“Fluid-dynamic drag” Metadata:

  • Title: Fluid-dynamic drag
  • Author:
  • Language: English
  • Publisher: ➤  Hoerner Fluid Dynamics - S.F. Hoerner
  • Publish Date:
  • Publish Location: ➤  Midland Park, N.J.] - [Midland Park, N.J.] - Vancouver, WA - Midland Park, N.J

“Fluid-dynamic drag” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1958
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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5Optimal pitch thrust-vector angle and benefits for all flight regimes

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“Optimal pitch thrust-vector angle and benefits for all flight regimes” Metadata:

  • Title: ➤  Optimal pitch thrust-vector angle and benefits for all flight regimes
  • Author:
  • Language: English
  • Number of Pages: Median: 22
  • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - Edwards, Calif

“Optimal pitch thrust-vector angle and benefits for all flight regimes” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 2000
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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    6The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil

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    “The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil” Metadata:

    • Title: ➤  The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil
    • Author:
    • Language: English
    • Number of Pages: Median: 18
    • Publisher: ➤  Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - For sale by the National Technical Information Service
    • Publish Date:
    • Publish Location: ➤  [Washington, D.C.] - Springfield, Va - Hampton, Va

    “The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil” 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

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      7In-flight transport performance optimization

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      “In-flight transport performance optimization” Metadata:

      • Title: ➤  In-flight transport performance optimization
      • Author:
      • Language: English
      • Number of Pages: Median: 15
      • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  [Springfield, Va - Edwards, Calif

      “In-flight transport performance optimization” 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:

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        8Viscous Drag Reduction

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        “Viscous Drag Reduction” Metadata:

        • Title: Viscous Drag Reduction
        • Author:
        • Language: English
        • Publisher: Plenum Press - Springer
        • Publish Date:

        “Viscous Drag Reduction” 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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        9Wave drag and high-speed performance of supersonic STOVL fighter configurations

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        “Wave drag and high-speed performance of supersonic STOVL fighter configurations” Metadata:

        • Title: ➤  Wave drag and high-speed performance of supersonic STOVL fighter configurations
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center
        • Publish Date:
        • Publish Location: Moffett Field, Calif

        “Wave drag and high-speed performance of supersonic STOVL fighter configurations” 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:

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          10Methods for estimating drag polars of subsonic airplanes

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          “Methods for estimating drag polars of subsonic airplanes” Metadata:

          • Title: ➤  Methods for estimating drag polars of subsonic airplanes
          • Author:
          • Language: English
          • Publish Date:
          • Publish Location: [Lawrence? Kan

          “Methods for estimating drag polars of subsonic airplanes” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1971
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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          11Drag reduction by shock and boundary layer control

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          Book's cover

          “Drag reduction by shock and boundary layer control” Metadata:

          • Title: ➤  Drag reduction by shock and boundary layer control
          • Author:
          • Language: English
          • Number of Pages: Median: 450
          • Publisher: ➤  Springer-Verlag GmbH u. Co.KG - Springer
          • Publish Date:
          • Publish Location: New York - Berlin

          “Drag reduction by shock and boundary layer control” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 2002
          • 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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            12Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44 ̊swept wing

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            “Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44 ̊swept wing” Metadata:

            • Title: ➤  Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44 ̊swept wing
            • Author:
            • Language: English
            • Number of Pages: Median: 35
            • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
            • Publish Date:
            • Publish Location: [Washington] - Springfield, Va

            “Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44 ̊swept wing” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

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

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            13Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers

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            “Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers” Metadata:

            • Title: ➤  Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers
            • Author:
            • Language: English
            • Number of Pages: Median: 162
            • 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

            “Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers” 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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            14Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)

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            “Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)” Metadata:

            • Title: ➤  Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)
            • Author:
            • Language: English
            • Number of Pages: Median: 209
            • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
            • Publish Date:
            • Publish Location: ➤  Washington, D.C - [Springfield, Va

            “Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)” 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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            15Flight-measured pressure characteristics of aft-facing steps in high Reynolds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data

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            “Flight-measured pressure characteristics of aft-facing steps in high Reynolds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data” Metadata:

            • Title: ➤  Flight-measured pressure characteristics of aft-facing steps in high Reynolds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data
            • Author:
            • Language: English
            • Number of Pages: Median: 35
            • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Office
            • Publish Date:
            • Publish Location: Springfield, Va - [Washington]

            “Flight-measured pressure characteristics of aft-facing steps in high Reynolds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

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

            Online Marketplaces

            Find Flight-measured pressure characteristics of aft-facing steps in high Reynolds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data at online marketplaces:


            16Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers

            By

            “Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers” Metadata:

            • Title: ➤  Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers
            • Author:
            • Language: English
            • Number of Pages: Median: 139
            • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch - Dryden Flight Research Facility
            • Publish Date:
            • Publish Location: ➤  Edwards, Cal - [Springfield, Va - [Washington, DC]

            “Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers” 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:

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              17The 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:

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                18A theory of gas-surface interactions at satellite velocities

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                “A theory of gas-surface interactions at satellite velocities” Metadata:

                • Title: ➤  A theory of gas-surface interactions at satellite velocities
                • Author:
                • Language: English
                • Number of Pages: Median: 76
                • Publisher: ➤  Institute for Aerospace Studies - [Institute for Aerospace Studies] - Institute for Aerospace Studies, University of Toronto]
                • Publish Date:
                • Publish Location: [Toronto - [Downsview, Ont.]

                “A theory of gas-surface interactions at satellite velocities” 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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                19Aerodynamic drag

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                “Aerodynamic drag” Metadata:

                • Title: Aerodynamic drag
                • Author:
                • Language: English
                • Number of Pages: Median: 259
                • Publish Date:
                • Publish Location: ➤  [Midland Park, N.J.] - [Midland Park? N. J.]

                “Aerodynamic drag” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1951
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

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                20Summary of studies to reduce wing-mounted propfan installation drag on an M=0.8 transport

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                “Summary of studies to reduce wing-mounted propfan installation drag on an M=0.8 transport” Metadata:

                • Title: ➤  Summary of studies to reduce wing-mounted propfan installation drag on an M=0.8 transport
                • Author:
                • Language: English
                • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
                • Publish Date:
                • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                “Summary of studies to reduce wing-mounted propfan installation drag on an M=0.8 transport” 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

                Online Access

                Downloads Are Not Available:

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                  21EUROSHOCK

                  By

                  “EUROSHOCK” Metadata:

                  • Title: EUROSHOCK
                  • Authors:
                  • Language: English
                  • Number of Pages: Median: 414
                  • Publisher: ➤  Vieweg - Friedrich Vieweg & Sohn Verlag
                  • Publish Date:
                  • Publish Location: Braunschweig/Wiesbaden

                  “EUROSHOCK” 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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                    22On the use of external burning to reduce aerospace vehicle transonic drag

                    By

                    “On the use of external burning to reduce aerospace vehicle transonic drag” Metadata:

                    • Title: ➤  On the use of external burning to reduce aerospace vehicle transonic drag
                    • Author:
                    • Language: English
                    • Number of Pages: Median: 14
                    • Publisher: ➤  For sale by the National Technical Information Service - NASA
                    • Publish Date:
                    • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                    “On the use of external burning to reduce aerospace vehicle transonic drag” 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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                    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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                      23Identification of intgrated airframe

                      By

                      “Identification of intgrated airframe” Metadata:

                      • Title: ➤  Identification of intgrated airframe
                      • 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: ➤  [Washington, DC] - [Springfield, Va

                      “Identification of intgrated airframe” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

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

                      Online Access

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                        24Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44ê swept wing

                        By

                        “Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44ê swept wing” Metadata:

                        • Title: ➤  Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44ê swept wing
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 35
                        • 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

                        “Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44ê swept wing” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

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

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                        Find Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44ê swept wing at online marketplaces:


                        25Experimental trim drag values and flow-field measurements for a wide-body transport model with conventional and supercritical wings

                        By

                        “Experimental trim drag values and flow-field measurements for a wide-body transport model with conventional and supercritical wings” Metadata:

                        • Title: ➤  Experimental trim drag values and flow-field measurements for a wide-body transport model with conventional and supercritical wings
                        • Author:
                        • Language: English
                        • Publisher: ➤  National Aeronautics and Space Administation, Scientific and Technical Information Branch
                        • Publish Date:
                        • Publish Location: [Washington, D.C.?]

                        “Experimental trim drag values and flow-field measurements for a wide-body transport model with conventional and supercritical wings” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1982
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

                        Online Access

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                          26Experimental and computational ice shapes and resulting drag increase for a NACA 0012 airfoil

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                          “Experimental and computational ice shapes and resulting drag increase for a NACA 0012 airfoil” Metadata:

                          • Title: ➤  Experimental and computational ice shapes and resulting drag increase for a NACA 0012 airfoil
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Aeronautics and Space Administration - For sale by the National Technical Information Service
                          • Publish Date:
                          • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                          “Experimental and computational ice shapes and resulting drag increase for a NACA 0012 airfoil” 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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                            27Applications of a direct/iterative design method to complex transonic configurations

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                            “Applications of a direct/iterative design method to complex transonic configurations” Metadata:

                            • Title: ➤  Applications of a direct/iterative design method to complex transonic configurations
                            • 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]

                            “Applications of a direct/iterative design method to complex transonic configurations” 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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                              28Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)

                              By

                              “Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)” Metadata:

                              • Title: ➤  Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)
                              • Author:
                              • Language: English
                              • Number of Pages: Median: 209
                              • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
                              • Publish Date:
                              • Publish Location: ➤  Washington, D.C - [Springfield, Va

                              “Full-scale wind-tunnel investigation of the advanced technology light twin-engine airplane (ATLIT)” Subjects and Themes:

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                              • First Year Published: 1980
                              • Is Full Text Available: No
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                              29Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers

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                              “Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers” Metadata:

                              • Title: ➤  Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers
                              • Author:
                              • Language: English
                              • Number of Pages: Median: 162
                              • 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

                              “Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers” Subjects and Themes:

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                              • First Year Published: 1984
                              • Is Full Text Available: No
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                              30Effect of afterbody geometry on aerodynamic characteristics of isolated nonaxisymmetric afterbodies at transonic Mach numbers

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                              “Effect of afterbody geometry on aerodynamic characteristics of isolated nonaxisymmetric afterbodies at transonic Mach numbers” Metadata:

                              • Title: ➤  Effect of afterbody geometry on aerodynamic characteristics of isolated nonaxisymmetric afterbodies at transonic Mach numbers
                              • 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]

                              “Effect of afterbody geometry on aerodynamic characteristics of isolated nonaxisymmetric afterbodies at transonic Mach numbers” Subjects and Themes:

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                              • First Year Published: 1992
                              • Is Full Text Available: No
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                                31Effects of tail span and empennage arrangement on drag of a typical single-engine fighter aft end

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                                “Effects of tail span and empennage arrangement on drag of a typical single-engine fighter aft end” Metadata:

                                • Title: ➤  Effects of tail span and empennage arrangement on drag of a typical single-engine fighter aft end
                                • 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.]

                                “Effects of tail span and empennage arrangement on drag of a typical single-engine fighter aft end” Subjects and Themes:

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

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                                  32Flight-measured pressure characteristics of aft-facing steps in high Reyonlds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data

                                  By

                                  “Flight-measured pressure characteristics of aft-facing steps in high Reyonlds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data” Metadata:

                                  • Title: ➤  Flight-measured pressure characteristics of aft-facing steps in high Reyonlds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data
                                  • Author:
                                  • Language: English
                                  • Number of Pages: Median: 35
                                  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Office
                                  • Publish Date:
                                  • Publish Location: Springfield, Va - [Washington]

                                  “Flight-measured pressure characteristics of aft-facing steps in high Reyonlds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data” Subjects and Themes:

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                                  • First Year Published: 1978
                                  • Is Full Text Available: No
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                                  33Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration

                                  By

                                  “Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration” Metadata:

                                  • Title: ➤  Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration
                                  • Author:
                                  • Language: English
                                  • Number of Pages: Median: 168
                                  • Publisher: ➤  Fo r sale by the National Technical Information Service] - National Aeronautics and Space Administrat ion, Scientific and Technical Information Branch
                                  • Publish Date:
                                  • Publish Location: ➤  Washington, D.C - [Springfield, Va

                                  “Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration” Subjects and Themes:

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                                  • First Year Published: 1979
                                  • Is Full Text Available: No
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                                  34Modification in drag of turbulent boundary layers resulting from manipulation of large-scale structures

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                                  “Modification in drag of turbulent boundary layers resulting from manipulation of large-scale structures” Metadata:

                                  • Title: ➤  Modification in drag of turbulent boundary layers resulting from manipulation of large-scale structures
                                  • Author:
                                  • Language: English
                                  • Number of Pages: Median: 25
                                  • 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

                                  “Modification in drag of turbulent boundary layers resulting from manipulation of large-scale structures” Subjects and Themes:

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                                  • First Year Published: 1981
                                  • Is Full Text Available: No
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                                  35Analytical and numerical investigation of structural response of compliant wall materials

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                                  “Analytical and numerical investigation of structural response of compliant wall materials” Metadata:

                                  • Title: ➤  Analytical and numerical investigation of structural response of compliant wall materials
                                  • Author:
                                  • Language: English
                                  • 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

                                  “Analytical and numerical investigation of structural response of compliant wall materials” Subjects and Themes:

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                                  Access and General Info:

                                  • First Year Published: 1978
                                  • Is Full Text Available: No
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                                  36Drag Reduction by Shock and Boundary Layer Control

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                                  “Drag Reduction by Shock and Boundary Layer Control” Metadata:

                                  • Title: ➤  Drag Reduction by Shock and Boundary Layer Control
                                  • Authors:
                                  • Language: English
                                  • Number of Pages: Median: 476
                                  • Publisher: ➤  Springer London, Limited - Brand: Springer - Springer Berlin Heidelberg
                                  • Publish Date:

                                  “Drag Reduction by Shock and Boundary Layer Control” Subjects and Themes:

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                                  Access and General Info:

                                  • First Year Published: 2010
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

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                                    37Aerodynamics of base combustion

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                                    “Aerodynamics of base combustion” Metadata:

                                    • Title: ➤  Aerodynamics of base combustion
                                    • Author: ➤  
                                    • Language: English
                                    • Number of Pages: Median: 522
                                    • Publisher: ➤  American Institute of Aeronautics and Astronautics
                                    • Publish Date:
                                    • Publish Location: New York

                                    “Aerodynamics of base combustion” Subjects and Themes:

                                    Edition Identifiers:

                                    Access and General Info:

                                    • First Year Published: 1976
                                    • Is Full Text Available: No
                                    • Is The Book Public: No
                                    • Access Status: No_ebook

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                                      38Aerodynamic Drag Mechanisms of Bluff Bodies and Road Vehicles

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                                      • Title: ➤  Aerodynamic Drag Mechanisms of Bluff Bodies and Road Vehicles
                                      • Author:
                                      • Language: English
                                      • Publisher: Springer US - Island Press
                                      • Publish Date:
                                      • Publish Location: Boston, MA

                                      “Aerodynamic Drag Mechanisms of Bluff Bodies and Road Vehicles” Subjects and Themes:

                                      Edition Identifiers:

                                      Access and General Info:

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

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                                        39Kinetic theory of resistance in rarefied gases

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                                        “Kinetic theory of resistance in rarefied gases” Metadata:

                                        • Title: ➤  Kinetic theory of resistance in rarefied gases
                                        • Author:
                                        • Language: English
                                        • Publish Date:

                                        “Kinetic theory of resistance in rarefied gases” Subjects and Themes:

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                                        • First Year Published: 1947
                                        • Is Full Text Available: No
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                                        40Some effects of base geometry on two dimensional base drag at subsonic and transonic speeds

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                                        “Some effects of base geometry on two dimensional base drag at subsonic and transonic speeds” Metadata:

                                        • Title: ➤  Some effects of base geometry on two dimensional base drag at subsonic and transonic speeds
                                        • Author:
                                        • Language: English
                                        • Number of Pages: Median: 19
                                        • Publisher: ➤  Dept. of Supply, Australian Defence Scientific Service, Aeronautical Research Laboratories
                                        • Publish Date:
                                        • Publish Location: Melbourne

                                        “Some effects of base geometry on two dimensional base drag at subsonic and transonic speeds” Subjects and Themes:

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                                        • First Year Published: 1969
                                        • Is Full Text Available: No
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                                        41A catalog of atmospheric densities from the drag on five artificial satellites

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                                        “A catalog of atmospheric densities from the drag on five artificial satellites” Metadata:

                                        • Title: ➤  A catalog of atmospheric densities from the drag on five artificial satellites
                                        • Author:
                                        • Language: English
                                        • Number of Pages: Median: 118
                                        • Publisher: ➤  Smithsonian Institution, Astrophysical Observatory
                                        • Publish Date:
                                        • Publish Location: Cambridge, Mass

                                        “A catalog of atmospheric densities from the drag on five artificial satellites” Subjects and Themes:

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

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                                        42Viscous drag reduction

                                        By

                                        “Viscous drag reduction” Metadata:

                                        • Title: Viscous drag reduction
                                        • Author: ➤  
                                        • Language: English
                                        • Number of Pages: Median: 500
                                        • Publisher: Plenum Press
                                        • Publish Date:
                                        • Publish Location: New York

                                        “Viscous drag reduction” Subjects and Themes:

                                        Edition Identifiers:

                                        • The Open Library ID: OL4563161M
                                        • Online Computer Library Center (OCLC) ID: 18635
                                        • Library of Congress Control Number (LCCN): 77076496

                                        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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                                        43Rotorcraft parasite drag

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                                        “Rotorcraft parasite drag” Metadata:

                                        • Title: Rotorcraft parasite drag
                                        • Author: ➤  
                                        • Language: English
                                        • Number of Pages: Median: 108
                                        • Publisher: The Committee
                                        • Publish Date:
                                        • Publish Location: Washington

                                        “Rotorcraft parasite drag” Subjects and Themes:

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                                        • First Year Published: 1975
                                        • Is Full Text Available: No
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                                        44The upper atmosphere and satellite drag

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                                        “The upper atmosphere and satellite drag” Metadata:

                                        • Title: ➤  The upper atmosphere and satellite drag
                                        • Author:
                                        • Language: English
                                        • Number of Pages: Median: 15
                                        • Publisher: Smithsonian Institution
                                        • Publish Date:
                                        • Publish Location: Washington

                                        “The upper atmosphere and satellite drag” Subjects and Themes:

                                        Edition Identifiers:

                                        • The Open Library ID: OL5814931M
                                        • Online Computer Library Center (OCLC) ID: 613259
                                        • Library of Congress Control Number (LCCN): 60062069

                                        Access and General Info:

                                        • First Year Published: 1960
                                        • Is Full Text Available: No
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                                        45An experimental investigation of the influence of base bleed on the base drag of various propelling nozzle configurations

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                                        “An experimental investigation of the influence of base bleed on the base drag of various propelling nozzle configurations” Metadata:

                                        • Title: ➤  An experimental investigation of the influence of base bleed on the base drag of various propelling nozzle configurations
                                        • Author: ➤  
                                        • Language: English
                                        • Number of Pages: Median: 25
                                        • Publisher: H.M.S.O.
                                        • Publish Date:
                                        • Publish Location: London

                                        “An experimental investigation of the influence of base bleed on the base drag of various propelling nozzle configurations” Subjects and Themes:

                                        Edition Identifiers:

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                                        • First Year Published: 1967
                                        • Is Full Text Available: No
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                                        46Flight 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:

                                        Access and General Info:

                                        • First Year Published: 1969
                                        • Is Full Text Available: No
                                        • Is The Book Public: No
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                                        47Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag

                                        By

                                        “Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag” Metadata:

                                        • Title: ➤  Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag
                                        • Author:
                                        • Language: English
                                        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Division - For sale by the National Technical Information Service]
                                        • Publish Date:
                                        • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                        “Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag” 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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                                          48Short-cowl front-fan turbojets; friction drag and wall-jet effects on cylindrical afterbodies

                                          By

                                          “Short-cowl front-fan turbojets; friction drag and wall-jet effects on cylindrical afterbodies” Metadata:

                                          • Title: ➤  Short-cowl front-fan turbojets; friction drag and wall-jet effects on cylindrical afterbodies
                                          • Author:
                                          • Language: English
                                          • Number of Pages: Median: 23
                                          • Publisher: H.M.S.O.
                                          • Publish Date:
                                          • Publish Location: London

                                          “Short-cowl front-fan turbojets; friction drag and wall-jet effects on cylindrical afterbodies” Subjects and Themes:

                                          Edition Identifiers:

                                          Access and General Info:

                                          • First Year Published: 1969
                                          • Is Full Text Available: No
                                          • Is The Book Public: No
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                                          49The pressure drag of an aerofoil with six different round leading edges, at transonic and low supersonic speeds

                                          By

                                          “The pressure drag of an aerofoil with six different round leading edges, at transonic and low supersonic speeds” Metadata:

                                          • Title: ➤  The pressure drag of an aerofoil with six different round leading edges, at transonic and low supersonic speeds
                                          • Author:
                                          • Language: English
                                          • Publisher: H.M.S.O.
                                          • Publish Date:
                                          • Publish Location: London

                                          “The pressure drag of an aerofoil with six different round leading edges, at transonic and low supersonic speeds” Subjects and Themes:

                                          Edition Identifiers:

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                                          • First Year Published: 1967
                                          • Is Full Text Available: No
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                                          50Drag on a body in nearly-free molecular flow

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                                          “Drag on a body in nearly-free molecular flow” Metadata:

                                          • Title: ➤  Drag on a body in nearly-free molecular flow
                                          • Author:
                                          • Language: English
                                          • Number of Pages: Median: 61
                                          • Publisher: ➤  Creative Media Partners, LLC - Courant Institute of Mathematical Sciences, New York University
                                          • Publish Date:
                                          • Publish Location: New York

                                          “Drag on a body in nearly-free molecular flow” Subjects and Themes:

                                          Edition Identifiers:

                                          Access and General Info:

                                          • First Year Published: 1963
                                          • Is Full Text Available: Yes
                                          • Is The Book Public: Yes
                                          • Access Status: Public

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                                            Wiki

                                            Source: Wikipedia

                                            Wikipedia Results

                                            Search Results from Wikipedia

                                            Drag (physics)

                                            waves. Last, in aerodynamics the term "parasitic drag" is often used. Parasitic drag is the sum of form drag and skin friction drag and is entirely negative

                                            Automotive aerodynamics

                                            Automotive aerodynamics is the study of the aerodynamics of road vehicles. Its main goals are reducing drag and wind noise, minimizing noise emission,

                                            Lift-to-drag ratio

                                            In aerodynamics, the lift-to-drag ratio (or L/D ratio) is the lift generated by an aerodynamic body such as an aerofoil or aircraft, divided by the aerodynamic

                                            Aerodynamics

                                            study of aerodynamics began in the modern sense in the eighteenth century, although observations of fundamental concepts such as aerodynamic drag were recorded

                                            Automobile drag coefficient

                                            The drag coefficient is a common measure in automotive design as it pertains to aerodynamics. Drag is a force that acts parallel to and in the same direction

                                            Lift-induced drag

                                            Lift-induced drag, induced drag, vortex drag, or sometimes drag due to lift, in aerodynamics, is an aerodynamic drag force that occurs whenever a moving

                                            Drag coefficient

                                            Clancy, L. J.: Aerodynamics. Section 11.17 Hoerner, Sighard F. (1965). Fluid-Dynamic Drag : Practical Information on Aerodynamic Drag and Hydrodynamic

                                            Drag curve

                                            The drag curve or drag polar is the relationship between the drag on an aircraft and other variables, such as lift, the coefficient of lift, angle-of-attack

                                            Parasitic drag

                                            {Re}}}} NACA duct Jet engine ram drag Skin friction line Anderson, John D. Jr. (1991). Fundamentals of aerodynamics (2nd ed.). New York: McGraw-Hill.

                                            Ground effect (aerodynamics)

                                            In aircraft, the ground effect is the reduced aerodynamic drag that an aircraft's wings generate when they are close to a surface (land or water). Ground