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1Numerical simulation of the SOFIA flowfield

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“Numerical simulation of the SOFIA flowfield” Metadata:

  • Title: ➤  Numerical simulation of the SOFIA flowfield
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
  • Publish Date:
  • Publish Location: ➤  Springfield, Va - [Washington, DC - San Jose, CA

“Numerical simulation of the SOFIA flowfield” 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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    22-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall

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    “2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” Metadata:

    • Title: ➤  2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
    • Author:
    • Language: English
    • Number of Pages: Median: 559
    • Publisher: ➤  National Technical Information Service, distributor - Ames Research Center - National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command
    • Publish Date:
    • Publish Location: ➤  Moffett Field, Calif - Moffett Field, Ca - [Springfield, Va

    “2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” 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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      3Control of unsteady separated flow associated with the dynamic stall of airfoils

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      “Control of unsteady separated flow associated with the dynamic stall of airfoils” Metadata:

      • Title: ➤  Control of unsteady separated flow associated with the dynamic stall of airfoils
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor - MCAT Institute
      • Publish Date:
      • Publish Location: ➤  Springfield, Va - [Washington, DC - Springfield, Va.? - San Jose, CA

      “Control of unsteady separated flow associated with the dynamic stall of airfoils” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

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

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        4Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight

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        “Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight” Metadata:

        • Title: ➤  Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight
        • Author:
        • Language: English
        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - Florida Atlantic University, Dept. of Mechanical Engineering, School of Engineering
        • Publish Date:
        • Publish Location: ➤  Boca Raton, FL - Springfield, Va - [Washington, DC

        “Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight” 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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          5Airfoil dynamic stall and rotorcraft maneuverability

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          “Airfoil dynamic stall and rotorcraft maneuverability” Metadata:

          • Title: ➤  Airfoil dynamic stall and rotorcraft maneuverability
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - Available from NASA Center for AeroSpace Information
          • Publish Date:
          • Publish Location: ➤  Hanover, MD - Moffett Field, Calif

          “Airfoil dynamic stall and rotorcraft maneuverability” 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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            6Study of the unsteady flow features on a stalled wing

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            “Study of the unsteady flow features on a stalled wing” Metadata:

            • Title: ➤  Study of the unsteady flow features on a stalled wing
            • Author:
            • Language: English
            • Publisher: ➤  American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration - National Technical Information Service, distributor
            • Publish Date:
            • Publish Location: ➤  Springfield, Va - Reston, VA - [Washington, DC

            “Study of the unsteady flow features on a stalled wing” 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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              7Evaluation of turbulence models for unsteady flows of an oscillating airfoil

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              “Evaluation of turbulence models for unsteady flows of an oscillating airfoil” Metadata:

              • Title: ➤  Evaluation of turbulence models for unsteady flows of an oscillating airfoil
              • Author:
              • Language: English
              • Publisher: ➤  Pergamon - National Technical Information Service, distributor] - National Aeronautics and Space Administration
              • Publish Date:
              • Publish Location: ➤  [New York] - [Washington, D.C - Springfield, Va

              “Evaluation of turbulence models for unsteady flows of an oscillating airfoil” 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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                8An analysis of the crossover between local and massive separation on airfoils

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                “An analysis of the crossover between local and massive separation on airfoils” Metadata:

                • Title: ➤  An analysis of the crossover between local and massive separation on airfoils
                • Author:
                • Number of Pages: Median: 103
                • Publisher: Langley Research Center
                • Publish Date:
                • Publish Location: Hampton, Va

                “An analysis of the crossover between local and massive separation on airfoils” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

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

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                9Aerodynamic simulation of ice accretion on airfoils

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                “Aerodynamic simulation of ice accretion on airfoils” Metadata:

                • Title: ➤  Aerodynamic simulation of ice accretion on airfoils
                • Author:
                • Language: English
                • Number of Pages: Median: 66
                • Publisher: ➤  National Aeronautics and Space Administration, Glenn Research Center
                • Publish Date:
                • Publish Location: Cleveland, Ohio

                “Aerodynamic simulation of ice accretion on airfoils” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 2011
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

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                  10Analysis of fully stalled compressor

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                  “Analysis of fully stalled compressor” Metadata:

                  • Title: ➤  Analysis of fully stalled compressor
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
                  • Publish Date:
                  • Publish Location: [Cleveland, Ohio

                  “Analysis of fully stalled compressor” 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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                  Downloads Are Not Available:

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                    11A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region

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                    “A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region” Metadata:

                    • Title: ➤  A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor
                    • Publish Date:
                    • Publish Location: Springfield, VA - Hampton, Va

                    “A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region” 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

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                      12Cellular structures in the flow over the flap of a two-element wing

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                      “Cellular structures in the flow over the flap of a two-element wing” Metadata:

                      • Title: ➤  Cellular structures in the flow over the flap of a two-element wing
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                      • Publish Date:
                      • Publish Location: ➤  [Washington, DC - Springfield, Va

                      “Cellular structures in the flow over the flap of a two-element wing” 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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                        13Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight

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                        “Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight” Metadata:

                        • Title: ➤  Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight
                        • Author:
                        • Language: English
                        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - Florida Atlantic University, Dept. of Mechanical Engineering, College of Engineering
                        • Publish Date:
                        • Publish Location: ➤  Boca Raton, FL - Springfield, Va - [Washington, DC

                        “Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight” 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

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                          14Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight

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                          “Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight” Metadata:

                          • Title: ➤  Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - Florida Atlantic University, Dept. of Mechanical Engineering, College of Engineering
                          • Publish Date:
                          • Publish Location: ➤  Boca Raton, FL - Springfield, Va - [Washington, DC

                          “Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight” 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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                            15Numerical simulation of dynamic stall of NACA0012 airfoil oscillating near static stall angle using the Navier-Stokes equations

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                            “Numerical simulation of dynamic stall of NACA0012 airfoil oscillating near static stall angle using the Navier-Stokes equations” Metadata:

                            • Title: ➤  Numerical simulation of dynamic stall of NACA0012 airfoil oscillating near static stall angle using the Navier-Stokes equations
                            • Author:
                            • Number of Pages: Median: 23
                            • Publisher: National Aerospace Laboratory
                            • Publish Date:
                            • Publish Location: Tokyo

                            “Numerical simulation of dynamic stall of NACA0012 airfoil oscillating near static stall angle using the Navier-Stokes equations” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

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

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                            16The phenomenon of dynamic stall

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                            “The phenomenon of dynamic stall” Metadata:

                            • Title: ➤  The phenomenon of dynamic stall
                            • Author:
                            • Publisher: Ames Research Center
                            • Publish Date:
                            • Publish Location: Moffett Field, Calif

                            “The phenomenon of dynamic stall” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

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

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                            17Some observations on transitory stall in conical diffusers

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                            “Some observations on transitory stall in conical diffusers” Metadata:

                            • Title: ➤  Some observations on transitory stall in conical diffusers
                            • Author:
                            • Language: English
                            • Publisher: Lewis Research Center
                            • Publish Date:
                            • Publish Location: Cleveland, Ohio

                            “Some observations on transitory stall in conical diffusers” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

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

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                              18Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane

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                              “Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane” Metadata:

                              • Title: ➤  Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane
                              • 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.]

                              “Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

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

                              Online Access

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                                19Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data

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                                “Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data” Metadata:

                                • Title: ➤  Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data
                                • Author:
                                • Language: English
                                • Number of Pages: Median: 63
                                • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
                                • Publish Date:
                                • Publish Location: Hampton, Va

                                “Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data” 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

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                                  20A description of the A.R.A. two-dimensional pitch and heave rig and some results from the NACA 0012 wing

                                  By

                                  “A description of the A.R.A. two-dimensional pitch and heave rig and some results from the NACA 0012 wing” Metadata:

                                  • Title: ➤  A description of the A.R.A. two-dimensional pitch and heave rig and some results from the NACA 0012 wing
                                  • Author:
                                  • Publisher: ➤  Aircraft Research Association Ltd
                                  • Publish Date:
                                  • Publish Location: Manton Lane, Bedford, England

                                  “A description of the A.R.A. two-dimensional pitch and heave rig and some results from the NACA 0012 wing” Subjects and Themes:

                                  Edition Identifiers:

                                  Access and General Info:

                                  • First Year Published: 1977
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

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                                  21The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data

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                                  “The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data” Metadata:

                                  • Title: ➤  The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data
                                  • Author:
                                  • Language: English
                                  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                  • Publish Date:
                                  • Publish Location: ➤  [Washington, D.C - Springfield, Va

                                  “The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data” 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

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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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                                    22Effect of acoustic excitation on stalled flows over an airfoil

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                                    “Effect of acoustic excitation on stalled flows over an airfoil” Metadata:

                                    • Title: ➤  Effect of acoustic excitation on stalled flows over an airfoil
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                    • Publish Date:
                                    • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                    “Effect of acoustic excitation on stalled flows over an airfoil” 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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                                      23A steadying effect of acoustic excitation on transitory stall

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                                      “A steadying effect of acoustic excitation on transitory stall” Metadata:

                                      • Title: ➤  A steadying effect of acoustic excitation on transitory stall
                                      • Author:
                                      • Language: English
                                      • Publisher: ➤  For sale by the National Technical Information Service, distributor - National Aeronautics and Space Administration
                                      • Publish Date:
                                      • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                      “A steadying effect of acoustic excitation on transitory stall” Subjects and Themes:

                                      Edition Identifiers:

                                      Access and General Info:

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

                                      Online Access

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                                        Wiki

                                        Source: Wikipedia

                                        Wikipedia Results

                                        Search Results from Wikipedia

                                        Stall (fluid dynamics)

                                        Stalling is caused by flow separation which, in turn, is caused by the air flowing against a rising pressure. Whitford describes three types of stall:

                                        Vortex generator

                                        contact with the airfoil surface, delays local flow separation and aerodynamic stalling, thereby improving the effectiveness of wings and control surfaces

                                        Stick shaker

                                        "stick") of an aircraft, warning the flight crew that an imminent aerodynamic stall has been detected. It is typically present on the majority of large

                                        Colgan Air Flight 3407

                                        Approaching Buffalo, the aircraft, a Bombardier Q400, entered an aerodynamic stall from which it did not recover and crashed into a house at 6038 Long

                                        Stall strips

                                        A stall strip is a small component fixed to the leading edge of the wing of an airplane to modify its aerodynamic characteristics. These stall strips may

                                        USAir Flight 427

                                        opposite to that commanded by the pilots, causing the plane to enter an aerodynamic stall from which Captain Peter Germano and First Officer Charles B. Emmet

                                        Stick pusher

                                        entering an aerodynamic stall. Some large fixed-wing aircraft display poor post-stall handling characteristics or are vulnerable to deep stall. To prevent

                                        Lauda Air Flight 004

                                        1 engine during the climb phase, causing the aircraft to enter an aerodynamic stall, uncontrolled dive, and in-flight breakup, killing all 213 passengers

                                        Chandelle

                                        heading at an airspeed in the "slow-flight" regime, very near the aerodynamic stall. The aircraft can be flown in "slow-flight" after establishing the

                                        Air France Flight 447

                                        miscommunication led to the pilots inadvertently stalling the Airbus A330. They failed to recover the aircraft from the stall, and the aircraft crashed into the mid-Atlantic