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Source: The Open Library

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1Lettin it all hang out

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Book's cover

“Lettin it all hang out” Metadata:

  • Title: Lettin it all hang out
  • Author:
  • Language: English
  • Number of Pages: Median: 227
  • Publisher: ➤  Hyperion - Hyperion Books (Adult Trd Pap) - Disney Press - Warner
  • Publish Date:
  • Publish Location: New York - London

“Lettin it all hang out” Subjects and Themes:

Edition Identifiers:

Access and General Info:

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

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2Dressing Up

Transvestism and Drag: The History of an Obsession

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Book's cover

“Dressing Up” Metadata:

  • Title: Dressing Up
  • Author:
  • Language: English
  • Number of Pages: Median: 160
  • Publisher: ➤  Simon and Schuster - Thames and Hudson - Thames and Hudson Ltd - Thames & Hudson
  • Publish Date:
  • Publish Location: London - New York

“Dressing Up” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1979
  • Is Full Text Available: Yes
  • Is The Book Public: No
  • Access Status: Borrowable

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3Two-dimensional converging-diverging rippled nozzles at transonic speeds

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“Two-dimensional converging-diverging rippled nozzles at transonic speeds” Metadata:

  • Title: ➤  Two-dimensional converging-diverging rippled nozzles at transonic speeds
  • Author:
  • Language: English
  • Number of Pages: Median: 105
  • Publisher: ➤  Langley Research Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
  • Publish Date:
  • Publish Location: ➤  Hampton - Hampton, Va - [Springfield, Va

“Two-dimensional converging-diverging rippled nozzles at transonic speeds” Subjects and Themes:

Edition Identifiers:

Access and General Info:

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

Online Access

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    4The 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

    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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      5How to Rob a Bank in Drag

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      Book's cover

      “How to Rob a Bank in Drag” Metadata:

      • Title: How to Rob a Bank in Drag
      • Authors:
      • Language: English
      • Number of Pages: Median: 377
      • Publisher: Images Outdoor, Inc.
      • Publish Date:
      • Publish Location: USA

      “How to Rob a Bank in Drag” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 2019
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

      Online Access

      Downloads Are Not Available:

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        6Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane

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        “Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane” Metadata:

        • Title: ➤  Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane
        • Author:
        • Language: English
        • Number of Pages: Median: 117
        • Publisher: ➤  For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Division
        • Publish Date:
        • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va - [Springfield,Va - Hampton, Va

        “Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane” 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

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          7In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)

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          “In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)” Metadata:

          • Title: ➤  In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
          • Publish Date:
          • Publish Location: ➤  [Springfield, Va - [Washington, DC]

          “In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

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

          Online Access

          Downloads Are Not Available:

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            8X-38 landing gear skid test report

            By

            “X-38 landing gear skid test report” Metadata:

            • Title: ➤  X-38 landing gear skid test report
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information (CASI)
            • Publish Date:
            • Publish Location: Hanover MD - Hampton, Va

            “X-38 landing gear skid test report” 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

            Online Access

            Downloads Are Not Available:

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              9Instability and transition of flow at, and near, an attachment-line

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              “Instability and transition of flow at, and near, an attachment-line” Metadata:

              • Title: ➤  Instability and transition of flow at, and near, an attachment-line
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Aeronautics and Space Administration - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: ➤  Hampton, Va - [Washington, DC - [Springfield, Va - Springfield, Va

              “Instability and transition of flow at, and near, an attachment-line” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

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

              Online Access

              Downloads Are Not Available:

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

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                10Sexuelle Verirrungen des Menschen und der Natur, 2. Teil

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                “Sexuelle Verirrungen des Menschen und der Natur, 2. Teil” Metadata:

                • Title: ➤  Sexuelle Verirrungen des Menschen und der Natur, 2. Teil
                • Author:
                • Language: ger
                • Number of Pages: Median: 418
                • Publisher: Standard-Verlag
                • Publish Date:
                • Publish Location: Berlin, Germany

                “Sexuelle Verirrungen des Menschen und der Natur, 2. Teil” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1910
                • 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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                  11A note on the total drag of jet flapeed wings

                  By

                  “A note on the total drag of jet flapeed wings” Metadata:

                  • Title: ➤  A note on the total drag of jet flapeed wings
                  • Author:
                  • Number of Pages: Median: 12
                  • Publisher: Institute of Aerophysics
                  • Publish Date:
                  • Publish Location: [Downsview, Ont.]

                  “A note on the total drag of jet flapeed wings” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1960
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

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                  12Flow distribution around the SSME main injector assembly using porosity formulation

                  By

                  “Flow distribution around the SSME main injector assembly using porosity formulation” Metadata:

                  • Title: ➤  Flow distribution around the SSME main injector assembly using porosity formulation
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                  • Publish Date:
                  • Publish Location: ➤  Springfield, Va - [Washington, DC

                  “Flow distribution around the SSME main injector assembly using porosity formulation” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

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

                  Online Access

                  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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                    13Influence of lift offset on rotorcraft performance

                    By

                    “Influence of lift offset on rotorcraft performance” Metadata:

                    • Title: ➤  Influence of lift offset on rotorcraft performance
                    • Author:
                    • Language: English
                    • Number of Pages: Median: 30
                    • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center
                    • Publish Date:
                    • Publish Location: Moffett Field, Calif

                    “Influence of lift offset on rotorcraft performance” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 2009
                    • 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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                      14Numerical analysis of a variable camber rotor blade as a lift cotrol device

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                      “Numerical analysis of a variable camber rotor blade as a lift cotrol device” Metadata:

                      • Title: ➤  Numerical analysis of a variable camber rotor blade as a lift cotrol device
                      • Author:
                      • Language: English
                      • Publisher: ➤  Flight Research Laboratory, University of Kansas Center for Research, Inc. - National Aeronautics and Space Administration, Ames Research Center
                      • Publish Date:
                      • Publish Location: ➤  [Moffett Field, Calif - Lawrence, Kans

                      “Numerical analysis of a variable camber rotor blade as a lift cotrol device” 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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                        15Technical status review on drag prediction and analysis from computational fluid dynamics

                        By

                        “Technical status review on drag prediction and analysis from computational fluid dynamics” Metadata:

                        • Title: ➤  Technical status review on drag prediction and analysis from computational fluid dynamics
                        • Author: ➤  
                        • Publisher: AGARD
                        • Publish Date:
                        • Publish Location: Neuilly sur Seine, France

                        “Technical status review on drag prediction and analysis from computational fluid dynamics” 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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                          163-D wake measurements near a hovering rotor for determining profile and induced drag

                          By

                          “3-D wake measurements near a hovering rotor for determining profile and induced drag” Metadata:

                          • Title: ➤  3-D wake measurements near a hovering rotor for determining profile and induced drag
                          • Author:
                          • Number of Pages: Median: 65
                          • Publisher: ➤  US Army Aviation and Troop Command, Aeroflightdynamics Directorate
                          • Publish Date:
                          • Publish Location: Moffett Field, Calif

                          “3-D wake measurements near a hovering rotor for determining profile and induced drag” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

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

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                          17In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisons with contemporary aircraft)

                          By

                          “In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisons with contemporary aircraft)” Metadata:

                          • Title: ➤  In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisons with contemporary aircraft)
                          • Author:
                          • Number of Pages: Median: 57
                          • Publisher: ➤  Dryden Flight Research Facility
                          • Publish Date:
                          • Publish Location: Edwards, Calif

                          “In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisons with contemporary aircraft)” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

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

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                          18Lift and drag of a wing spanning a free jet

                          By

                          “Lift and drag of a wing spanning a free jet” Metadata:

                          • Title: ➤  Lift and drag of a wing spanning a free jet
                          • Author:
                          • Publisher: HMSO
                          • Publish Date:
                          • Publish Location: London

                          “Lift and drag of a wing spanning a free jet” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1934
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

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                          19Crew emergency return vehicle autoland feasibility study

                          By

                          “Crew emergency return vehicle autoland feasibility study” Metadata:

                          • Title: ➤  Crew emergency return vehicle autoland feasibility study
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                          • Publish Date:
                          • Publish Location: Hampton, Va - [Springfield, Va

                          “Crew emergency return vehicle autoland feasibility study” 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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                            20On the lift and induced drag associated with large downwash angles

                            By

                            “On the lift and induced drag associated with large downwash angles” Metadata:

                            • Title: ➤  On the lift and induced drag associated with large downwash angles
                            • Author:
                            • Number of Pages: Median: 15
                            • Publisher: Institute of Aerophysics
                            • Publish Date:
                            • Publish Location: [Downsview, Ont.]

                            “On the lift and induced drag associated with large downwash angles” 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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                            21Study of the TRAC airfoil table computational system

                            By

                            “Study of the TRAC airfoil table computational system” Metadata:

                            • Title: ➤  Study of the TRAC airfoil table computational system
                            • Author:
                            • Language: English
                            • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                            • Publish Date:
                            • Publish Location: Hampton, Va - [Springfield, Va

                            “Study of the TRAC airfoil table computational system” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1999
                            • 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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                              22Further studies on the 21% thick, supercritical NLR airfoil NAE 68-060-21:1

                              By

                              “Further studies on the 21% thick, supercritical NLR airfoil NAE 68-060-21:1” Metadata:

                              • Title: ➤  Further studies on the 21% thick, supercritical NLR airfoil NAE 68-060-21:1
                              • Author:
                              • Number of Pages: Median: 27
                              • Publisher: ➤  National Aeronautical Establishment
                              • Publish Date:
                              • Publish Location: Ottawa

                              “Further studies on the 21% thick, supercritical NLR airfoil NAE 68-060-21:1” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

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

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                              23Control theory based airfoil design using the Euler equations

                              By

                              “Control theory based airfoil design using the Euler equations” Metadata:

                              • Title: ➤  Control theory based airfoil design using the Euler equations
                              • Author:
                              • Language: English
                              • Publisher: ➤  Research Institute for Advanced Computer Science, NASA Ames Research Center - National Technical Information Service, distributor
                              • Publish Date:
                              • Publish Location: ➤  [Moffett Field, Calif.] - [Springfield, Va

                              “Control theory based airfoil design using the Euler equations” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

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

                              Online Access

                              Downloads Are Not Available:

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

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                                24A comparison of approximate methods of predicting shock detachment distance for two-dimensional supersonic inlets

                                By

                                “A comparison of approximate methods of predicting shock detachment distance for two-dimensional supersonic inlets” Metadata:

                                • Title: ➤  A comparison of approximate methods of predicting shock detachment distance for two-dimensional supersonic inlets
                                • Author:
                                • Number of Pages: Median: 47
                                • Publisher: ➤  Faculty of the School of Engineering, Air Force Institute of Technology, Air University
                                • Publish Date:
                                • Publish Location: ➤  Wright-Patterson Air Force Base, Ohio

                                “A comparison of approximate methods of predicting shock detachment distance for two-dimensional supersonic inlets” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

                                • First Year Published: 1974
                                • Is Full Text Available: No
                                • Is The Book Public: No
                                • Access Status: No_ebook

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                                25The drag of spheres at porosites ranging from an isolated sphere to a packed bed

                                By

                                “The drag of spheres at porosites ranging from an isolated sphere to a packed bed” Metadata:

                                • Title: ➤  The drag of spheres at porosites ranging from an isolated sphere to a packed bed
                                • Author:
                                • Number of Pages: Median: 11
                                • Publisher: ➤  College of Aeronautics, Cranfield Institute of Technology
                                • Publish Date:
                                • Publish Location: Cranfield, Bedford

                                “The drag of spheres at porosites ranging from an isolated sphere to a packed bed” 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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                                26Experiments on the lift and drag of spheres suspended in a Poiseuille flow

                                By

                                “Experiments on the lift and drag of spheres suspended in a Poiseuille flow” Metadata:

                                • Title: ➤  Experiments on the lift and drag of spheres suspended in a Poiseuille flow
                                • Author:
                                • Number of Pages: Median: 32
                                • Publisher: ➤  Dept. of Aerospace Engineering, School of Engineering and Applied Science, University of Virginia
                                • Publish Date:
                                • Publish Location: Charlottesville, Va

                                “Experiments on the lift and drag of spheres suspended in a Poiseuille flow” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

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

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                                27Numerical and experimental study of drag characteristics of two-dimensional HLFC airfoils in high subsonic, high Reynolds number flow

                                By

                                “Numerical and experimental study of drag characteristics of two-dimensional HLFC airfoils in high subsonic, high Reynolds number flow” Metadata:

                                • Title: ➤  Numerical and experimental study of drag characteristics of two-dimensional HLFC airfoils in high subsonic, high Reynolds number flow
                                • Author:
                                • Number of Pages: Median: 12
                                • Publisher: National Aerospace Laboratory
                                • Publish Date:
                                • Publish Location: Chofu, Tokyo

                                “Numerical and experimental study of drag characteristics of two-dimensional HLFC airfoils in high subsonic, high Reynolds number flow” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

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

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                                28Get Started with Microsoft PowerPoint 97! - Illustrated Interactive

                                By

                                “Get Started with Microsoft PowerPoint 97! - Illustrated Interactive” Metadata:

                                • Title: ➤  Get Started with Microsoft PowerPoint 97! - Illustrated Interactive
                                • Author:
                                • Language: English
                                • Number of Pages: Median: 80
                                • Publisher: Course Technology
                                • Publish Date:

                                “Get Started with Microsoft PowerPoint 97! - Illustrated Interactive” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

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

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                                  29Transvestism Around the World

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                                  “Transvestism Around the World” Metadata:

                                  • Title: Transvestism Around the World
                                  • Author:
                                  • Language: English
                                  • Publisher: S-K Press
                                  • Publish Date:
                                  • Publish Location: New York, NY, USA

                                  “Transvestism Around the World” Subjects and Themes:

                                  Edition Identifiers:

                                  Access and General Info:

                                  • First Year Published: 1964
                                  • Is Full Text Available: Yes
                                  • Is The Book Public: Yes
                                  • Access Status: Public

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