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Source: The Open Library

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1Low-speed wind-tunnel test of a STOL supersonic-cruise fighter concept

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“Low-speed wind-tunnel test of a STOL supersonic-cruise fighter concept” Metadata:

  • Title: ➤  Low-speed wind-tunnel test of a STOL supersonic-cruise fighter concept
  • Author:
  • Language: English
  • Number of Pages: Median: 41
  • Publisher: ➤  Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Division - For sale by the National Technical Information Service]
  • Publish Date:
  • Publish Location: ➤  Hampton, Va - [Washington, DC] - [Springfield, Va

“Low-speed wind-tunnel test of a STOL supersonic-cruise fighter concept” 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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    2Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept

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    “Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept” Metadata:

    • Title: ➤  Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
    • Author:
    • Language: English
    • Number of Pages: Median: 36
    • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Langley Research Center - For sale by the National Technical Information Service]
    • Publish Date:
    • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, D.C.]

    “Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept” 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:

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      3Powered-lift aircraft technology

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      “Powered-lift aircraft technology” Metadata:

      • Title: ➤  Powered-lift aircraft technology
      • Author:
      • Language: English
      • Number of Pages: Median: 36
      • Publisher: ➤  NASA - For sale by the Supt. of Docs., U.S. G.P.O. - Scientific and Technical Information Branch, National Aeronautics and Space Administration - Scientific and Technical Information Division, National Aeronautics and Space Administration
      • Publish Date:
      • Publish Location: ➤  Washington, D. C - Washington, DC

      “Powered-lift aircraft technology” 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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      4Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft

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      “Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft” Metadata:

      • Title: ➤  Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft
      • Author:
      • Language: English
      • Number of Pages: Median: 10
      • Publisher: ➤  For sale by the National Technical Information Service - NASA
      • Publish Date:
      • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

      “Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft” 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

      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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        5Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration

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        “Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration” Metadata:

        • Title: ➤  Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration
        • Author:
        • Language: English
        • Number of Pages: Median: 28
        • Publisher: ➤  Langley Research Center - For sale by the National Technical Information Service - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
        • Publish Date:
        • Publish Location: ➤  Springfield, Va - Hampton, Va - [Washington, D.C.]

        “Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration” 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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          6Flight investigation of the use of a nose gear jump strut to reduce takeoff ground roll distance of STOL aircraft

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          “Flight investigation of the use of a nose gear jump strut to reduce takeoff ground roll distance of STOL aircraft” Metadata:

          • Title: ➤  Flight investigation of the use of a nose gear jump strut to reduce takeoff ground roll distance of STOL aircraft
          • Author:
          • Language: English
          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
          • Publish Date:
          • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va

          “Flight investigation of the use of a nose gear jump strut to reduce takeoff ground roll distance of STOL 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

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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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            7Supersonic flow computations for an ASTOVL aircraft configuration

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            “Supersonic flow computations for an ASTOVL aircraft configuration” Metadata:

            • Title: ➤  Supersonic flow computations for an ASTOVL aircraft configuration
            • Author:
            • Language: English
            • Number of Pages: Median: 40
            • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center
            • Publish Date:
            • Publish Location: ➤  [Washington, D.C.] - Hampton, Va

            “Supersonic flow computations for an ASTOVL aircraft configuration” 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

            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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              8Performance, operation and use of low aspect ratio jet flapped wings

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              “Performance, operation and use of low aspect ratio jet flapped wings” Metadata:

              • Title: ➤  Performance, operation and use of low aspect ratio jet flapped wings
              • Author:
              • Number of Pages: Median: 18
              • Publisher: ➤  Institute for Aerospace Studies
              • Publish Date:
              • Publish Location: [Downsview, Ont.]

              “Performance, operation and use of low aspect ratio jet flapped wings” 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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              9The application of techniques for predicting STOL aircraft response to wind shear and turbulence during the landing approach

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              “The application of techniques for predicting STOL aircraft response to wind shear and turbulence during the landing approach” Metadata:

              • Title: ➤  The application of techniques for predicting STOL aircraft response to wind shear and turbulence during the landing approach
              • Author:
              • Publisher: ➤  Institute for Aerospace Studies
              • Publish Date:
              • Publish Location: [Downsview, Ont.]

              “The application of techniques for predicting STOL aircraft response to wind shear and turbulence during the landing approach” 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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              10Development and application of computational techniques for handling the lateral STOL aircraft response to crosswind shear and turbulence during a landing approach in the planetary boundary layer

              By

              “Development and application of computational techniques for handling the lateral STOL aircraft response to crosswind shear and turbulence during a landing approach in the planetary boundary layer” Metadata:

              • Title: ➤  Development and application of computational techniques for handling the lateral STOL aircraft response to crosswind shear and turbulence during a landing approach in the planetary boundary layer
              • Author:
              • Publisher: ➤  Dept. of Aerospace Science and Engineering
              • Publish Date:
              • Publish Location: [Downsview, Ont.]

              “Development and application of computational techniques for handling the lateral STOL aircraft response to crosswind shear and turbulence during a landing approach in the planetary boundary layer” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

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

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              11Microwave landing system requirements for STOL operations

              By

              “Microwave landing system requirements for STOL operations” Metadata:

              • Title: ➤  Microwave landing system requirements for STOL operations
              • Author:
              • Number of Pages: Median: 11
              • Publisher: ➤  American Institute of Aeronautics and Astronautics
              • Publish Date:
              • Publish Location: New York

              “Microwave landing system requirements for STOL operations” 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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              12Considerations for STOL landing ground rules

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              “Considerations for STOL landing ground rules” Metadata:

              • Title: ➤  Considerations for STOL landing ground rules
              • Author:
              • Number of Pages: Median: 12
              • Publisher: ➤  American Institute of Aeronautics and Astronautics
              • Publish Date:
              • Publish Location: New York

              “Considerations for STOL landing ground rules” 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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              13A statistical analysis of pilot control during a simulation of STOL landing approaches

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              “A statistical analysis of pilot control during a simulation of STOL landing approaches” Metadata:

              • Title: ➤  A statistical analysis of pilot control during a simulation of STOL landing approaches
              • Author:
              • Publisher: ➤  American Institute of Aeronautics and Astronautics
              • Publish Date:
              • Publish Location: Washington, D. C

              “A statistical analysis of pilot control during a simulation of STOL landing approaches” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1973
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

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              14ASTOVL combat aircraft design synthesis and optimization

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              “ASTOVL combat aircraft design synthesis and optimization” Metadata:

              • Title: ➤  ASTOVL combat aircraft design synthesis and optimization
              • Author:
              • Number of Pages: Median: 267
              • Publisher: ➤  Cranfield Institute of Technology, College of Aeronautics
              • Publish Date:
              • Publish Location: Cranfield, Bedford, England

              “ASTOVL combat aircraft design synthesis and optimization” 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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              15STOVL propulsion system volume dynamics approximations

              By

              “STOVL propulsion system volume dynamics approximations” Metadata:

              • Title: ➤  STOVL propulsion system volume dynamics approximations
              • Author:
              • Language: English
              • Publisher: Lewis Research Center
              • Publish Date:
              • Publish Location: Cleveland, Ohio

              “STOVL propulsion system volume dynamics approximations” 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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                16A STOL airworthiness investigation using a simulation of a deflected slipstream transport

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                “A STOL airworthiness investigation using a simulation of a deflected slipstream transport” Metadata:

                • Title: ➤  A STOL airworthiness investigation using a simulation of a deflected slipstream transport
                • Author:
                • Publisher: Ames Research Center
                • Publish Date:
                • Publish Location: Moffett Field, Calif

                “A STOL airworthiness investigation using a simulation of a deflected slipstream transport” 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

                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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                  17A case study in aircraft design

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                  “A case study in aircraft design” Metadata:

                  • Title: ➤  A case study in aircraft design
                  • Author:
                  • Publisher: AIAA
                  • Publish Date:
                  • Publish Location: New York

                  “A case study in aircraft design” 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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                  18On the lift and induced drag associated with large downwash angles

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                  “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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                  19Internal performance of highly integrated deployable exhaust nozzles applicable to advanced short-takeoff and vertical-landing aircraft

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                  “Internal performance of highly integrated deployable exhaust nozzles applicable to advanced short-takeoff and vertical-landing aircraft” Metadata:

                  • Title: ➤  Internal performance of highly integrated deployable exhaust nozzles applicable to advanced short-takeoff and vertical-landing aircraft
                  • Author:
                  • Number of Pages: Median: 277
                  • Publisher: Langley Research Center
                  • Publish Date:
                  • Publish Location: Hampton, Va

                  “Internal performance of highly integrated deployable exhaust nozzles applicable to advanced short-takeoff and vertical-landing aircraft” 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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                  20Evaluation of four advanced nozzle concepts for short takeoff and landing performance

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                  “Evaluation of four advanced nozzle concepts for short takeoff and landing performance” Metadata:

                  • Title: ➤  Evaluation of four advanced nozzle concepts for short takeoff and landing performance
                  • Author:
                  • Number of Pages: Median: 95
                  • Publisher: Langley Research Center
                  • Publish Date:
                  • Publish Location: Hampton, Va

                  “Evaluation of four advanced nozzle concepts for short takeoff and landing performance” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

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

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                  21V/STOL aircraft configurations and opportunities in the Pacific Basin

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                  “V/STOL aircraft configurations and opportunities in the Pacific Basin” Metadata:

                  • Title: ➤  V/STOL aircraft configurations and opportunities in the Pacific Basin
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
                  • Publish Date:
                  • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va

                  “V/STOL aircraft configurations and opportunities in the Pacific Basin” 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:

                  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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                    22Velocity and temperature decay characteristics of inverted-profile jets

                    By

                    “Velocity and temperature decay characteristics of inverted-profile jets” Metadata:

                    • Title: ➤  Velocity and temperature decay characteristics of inverted-profile jets
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
                    • Publish Date:
                    • Publish Location: [Cleveland, Ohio

                    “Velocity and temperature decay characteristics of inverted-profile jets” 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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                      23Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability

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                      “Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability” Metadata:

                      • Title: ➤  Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability
                      • 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.]

                      “Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

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

                      Online Access

                      Downloads Are Not Available:

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

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                        24STOVL aircraft simulation for integrated flight and propulsion controls research

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                        “STOVL aircraft simulation for integrated flight and propulsion controls research” Metadata:

                        • Title: ➤  STOVL aircraft simulation for integrated flight and propulsion controls research
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 21
                        • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Lewis Research Center
                        • Publish Date:
                        • Publish Location: ➤  [Cleveland, Ohio?] - [Springfield, Va

                        “STOVL aircraft simulation for integrated flight and propulsion controls research” 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

                        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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                          25STOL-V/STOL city center transport aircraft study

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                          “STOL-V/STOL city center transport aircraft study” Metadata:

                          • Title: ➤  STOL-V/STOL city center transport aircraft study
                          • Author:
                          • Number of Pages: Median: 168
                          • Publisher: McDonnell Aircraft Corporation
                          • Publish Date:
                          • Publish Location: St. Louis Mo

                          “STOL-V/STOL city center transport aircraft study” 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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                          26A study of lateral flight path perturbations of STOL aircraft in the planetary boundary layer

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                          “A study of lateral flight path perturbations of STOL aircraft in the planetary boundary layer” Metadata:

                          • Title: ➤  A study of lateral flight path perturbations of STOL aircraft in the planetary boundary layer
                          • Author:
                          • Publisher: ➤  Institute for Aerospace Studies
                          • Publish Date:
                          • Publish Location: [Downsview, Ont.]

                          “A study of lateral flight path perturbations of STOL aircraft in the planetary boundary layer” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

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

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                          27Design and analysis of a longitudinal ride comfort control system for a short take-off and landing (STOL) aircraft

                          By

                          “Design and analysis of a longitudinal ride comfort control system for a short take-off and landing (STOL) aircraft” Metadata:

                          • Title: ➤  Design and analysis of a longitudinal ride comfort control system for a short take-off and landing (STOL) aircraft
                          • Author:
                          • Number of Pages: Median: 74
                          • Publisher: ➤  Dept. of Aerospace Science and Engineering
                          • Publish Date:
                          • Publish Location: [Downsview, Ont.]

                          “Design and analysis of a longitudinal ride comfort control system for a short take-off and landing (STOL) aircraft” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

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

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                          28Design and analysis of longitudinal ride comfort control system for a short take-off and landing (STOL) aircraft

                          By

                          “Design and analysis of longitudinal ride comfort control system for a short take-off and landing (STOL) aircraft” Metadata:

                          • Title: ➤  Design and analysis of longitudinal ride comfort control system for a short take-off and landing (STOL) aircraft
                          • Author:
                          • Number of Pages: Median: 72
                          • Publisher: ➤  Institute for Aerospace Studies
                          • Publish Date:
                          • Publish Location: [Downsview, Ont.]

                          “Design and analysis of longitudinal ride comfort control system for a short take-off and landing (STOL) aircraft” 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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                          29Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA)

                          By

                          “Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA)” Metadata:

                          • Title: ➤  Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA)
                          • Author:
                          • Number of Pages: Median: 38
                          • Publisher: Ames Research Center
                          • Publish Date:
                          • Publish Location: Moffett Field, Calif

                          “Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA)” 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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                          30An assessment of STOL technology

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                          “An assessment of STOL technology” Metadata:

                          • Title: ➤  An assessment of STOL technology
                          • Author:
                          • Publisher: ➤  Institute for Aerospace Studies
                          • Publish Date:
                          • Publish Location: [Downsview, Ont.]

                          “An assessment of STOL technology” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

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

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                          31STOL technology bibliography update

                          By

                          “STOL technology bibliography update” Metadata:

                          • Title: ➤  STOL technology bibliography update
                          • Author:
                          • Publisher: ➤  Institute for Aerospace Studies
                          • Publish Date:
                          • Publish Location: [Downsview, Ont.]

                          “STOL technology bibliography update” 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

                          Online Marketplaces

                          Find STOL technology bibliography update at online marketplaces:


                          32A review and application of the equivalent deterministic variable technique

                          By

                          “A review and application of the equivalent deterministic variable technique” Metadata:

                          • Title: ➤  A review and application of the equivalent deterministic variable technique
                          • Author:
                          • Publisher: ➤  Institute for Aerospace Studies
                          • Publish Date:
                          • Publish Location: [Downsview, Ont.]

                          “A review and application of the equivalent deterministic variable technique” 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 A review and application of the equivalent deterministic variable technique at online marketplaces:



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                          Wiki

                          Source: Wikipedia

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                          STOL

                          A short takeoff and landing (STOL) aircraft is a fixed-wing aircraft that can takeoff/land on short runways. Many STOL-designed aircraft can operate on

                          Takeoff

                          Takeoff is the phase of flight in which an aerospace vehicle leaves the ground and becomes airborne. For aircraft traveling vertically, this is known

                          VTOL

                          wingtip. The Osprey is a multi-mission aircraft with both a vertical takeoff and landing (VTOL) and short takeoff and landing capability (STOL). It is designed

                          V/STOL

                          and/or short take-off and landing (V/STOL) aircraft is an airplane able to take off or land vertically or on short runways. Vertical takeoff and landing

                          Maximum takeoff weight

                          The maximum takeoff weight (MTOW) or maximum gross takeoff weight (MGTOW) or maximum takeoff mass (MTOM) of an aircraft, also known as the maximum structural

                          Takeoff and landing

                          speed. Some airplanes can take off at low speed, this being a short takeoff. Some aircraft such as helicopters and Harrier jump jets can take off and land

                          Rejected takeoff

                          Reasons to perform a rejected takeoff vary but are usually related to a suspected or actual problem with the aircraft, such as an engine failure; fire;

                          List of STOL aircraft

                          list of aircraft which are classified as having Short Takeoff and Landing, or STOL, characteristics. The STOL class excludes vertical takeoff and landing

                          Takeoff/go-around switch

                          A takeoff/go-around switch (TO/GA or TOGA; /ˈtoʊɡə/) is a switch on the autothrottle of modern large aircraft, with two modes: takeoff (TO) and go-around

                          STOVL

                          run, and capable of landing vertically. On aircraft carriers, non-catapult-assisted fixed-wing short takeoffs are accomplished with the use of thrust vectoring


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