Explore: Lateral Stability Of Airplanes

Discover books, insights, and more — all in one place.

Learn more about Lateral Stability Of Airplanes with top reads curated from trusted sources — all in one place.

Topic Search

Search for any topic

AI-Generated Overview About “lateral-stability-of-airplanes”:


Books Results

Source: The Open Library

The Open Library Search Results

Search results from The Open Library

1Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack

By

“Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack” Metadata:

  • Title: ➤  Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack
  • Author:
  • Language: English
  • Number of Pages: Median: 35
  • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center - National Technical Information Service, distributor]
  • Publish Date:
  • Publish Location: ➤  [Washington, D.C] - [Springfield, Va - [Washington, D.C.]

“Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack” Subjects and Themes:

Edition Identifiers:

Access and General Info:

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

Online Access

Downloads Are Not Available:

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

Online Borrowing:

    Online Marketplaces

    Find Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack at online marketplaces:


    2X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data

    By

    “X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data” Metadata:

    • Title: ➤  X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data
    • Author:
    • Language: English
    • Number of Pages: Median: 35
    • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center - National Aeronautics and Space Administration - National Technical Information Service, distributor]
    • Publish Date:
    • Publish Location: ➤  [Washington, D.C] - Washington, D.C - [Springfield, Va - [Washington, D.C.]

    “X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight 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

    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.

    Online Borrowing:

      Online Marketplaces

      Find X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data at online marketplaces:


      3Effects of cockpit lateral stick characteristics on handling qualities and pilot dynamics

      By

      “Effects of cockpit lateral stick characteristics on handling qualities and pilot dynamics” Metadata:

      • Title: ➤  Effects of cockpit lateral stick characteristics on handling qualities and pilot dynamics
      • Authors:
      • Language: English
      • Number of Pages: Median: 203
      • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - Dryden Flight Research Facility - National Technical Information Service, distributor]
      • Publish Date:
      • Publish Location: ➤  [Springfield, Va.? - [Washington, D.C.] - Washington

      “Effects of cockpit lateral stick characteristics on handling qualities and pilot dynamics” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

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

      Online Access

      Downloads Are Not Available:

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

      Online Borrowing:

        Online Marketplaces

        Find Effects of cockpit lateral stick characteristics on handling qualities and pilot dynamics at online marketplaces:


        4Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)

        By

        “Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)” Metadata:

        • Title: ➤  Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)
        • Author:
        • Language: English
        • Number of Pages: Median: 32
        • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

        “Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)” 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.

        Online Borrowing:

          Online Marketplaces

          Find Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA) at online marketplaces:


          5Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration

          By

          “Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration” Metadata:

          • Title: ➤  Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration
          • Author:
          • Language: English
          • Number of Pages: Median: 30
          • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center
          • Publish Date:
          • Publish Location: ➤  Hampton, Va - [Springfield, Va - Washington, D.C

          “Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration” 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.

          Online Borrowing:

            Online Marketplaces

            Find Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration at online marketplaces:


            6Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds

            By

            “Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds” Metadata:

            • Title: ➤  Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds
            • Author:
            • Language: English
            • Number of Pages: Median: 197
            • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
            • Publish Date:
            • Publish Location: ➤  [Springfield, Va - Washington, D.C

            “Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds” 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

            Online Marketplaces

            Find Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds at online marketplaces:


            7A simulator investigation of rolling requirements for landing approach

            By

            “A simulator investigation of rolling requirements for landing approach” Metadata:

            • Title: ➤  A simulator investigation of rolling requirements for landing approach
            • Author:
            • Language: English
            • Number of Pages: Median: 37
            • Publisher: H.M. Stationery Off.
            • Publish Date:
            • Publish Location: London

            “A simulator investigation of rolling requirements for landing approach” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

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

            Online Marketplaces

            Find A simulator investigation of rolling requirements for landing approach at online marketplaces:


            8Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds

            By

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

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

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

            Edition Identifiers:

            Access and General Info:

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

            Online Marketplaces

            Find Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds at online marketplaces:


            9Flight assessment of a variable-stability helicopter for STOL simulations and evaluation of the influence of several lateral-directional stability derivatives

            By

            “Flight assessment of a variable-stability helicopter for STOL simulations and evaluation of the influence of several lateral-directional stability derivatives” Metadata:

            • Title: ➤  Flight assessment of a variable-stability helicopter for STOL simulations and evaluation of the influence of several lateral-directional stability derivatives
            • Author:
            • Language: English
            • Number of Pages: Median: 23
            • Publisher: ➤  National Research Council of Canada
            • Publish Date:
            • Publish Location: [Ottawa

            “Flight assessment of a variable-stability helicopter for STOL simulations and evaluation of the influence of several lateral-directional stability derivatives” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

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

            Online Marketplaces

            Find Flight assessment of a variable-stability helicopter for STOL simulations and evaluation of the influence of several lateral-directional stability derivatives at online marketplaces:


            10Interim report on low-speed flight tests of a slender-wing research aircraft (Handley Page H. P. 115)

            By

            “Interim report on low-speed flight tests of a slender-wing research aircraft (Handley Page H. P. 115)” Metadata:

            • Title: ➤  Interim report on low-speed flight tests of a slender-wing research aircraft (Handley Page H. P. 115)
            • Author:
            • Language: English
            • Number of Pages: Median: 30
            • Publisher: H.M.S.O.
            • Publish Date:
            • Publish Location: London

            “Interim report on low-speed flight tests of a slender-wing research aircraft (Handley Page H. P. 115)” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

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

            Online Marketplaces

            Find Interim report on low-speed flight tests of a slender-wing research aircraft (Handley Page H. P. 115) at online marketplaces:


            11A review of recent research on handling qualities, and its application to the handling problems of large aircraft

            By

            “A review of recent research on handling qualities, and its application to the handling problems of large aircraft” Metadata:

            • Title: ➤  A review of recent research on handling qualities, and its application to the handling problems of large aircraft
            • Author:
            • Language: English
            • Number of Pages: Median: 42
            • Publisher: H.M.S.O.
            • Publish Date:
            • Publish Location: London

            “A review of recent research on handling qualities, and its application to the handling problems of large aircraft” Subjects and Themes:

            Edition Identifiers:

            • The Open Library ID: OL5588282M
            • Online Computer Library Center (OCLC) ID: 6188557
            • Library of Congress Control Number (LCCN): 67108682

            Access and General Info:

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

            Online Marketplaces

            Find A review of recent research on handling qualities, and its application to the handling problems of large aircraft at online marketplaces:


            12Directional stability in flight with bank angle constraint as a condition defining a minimum acceptable value for n[superscript v]

            By

            “Directional stability in flight with bank angle constraint as a condition defining a minimum acceptable value for n[superscript v]” Metadata:

            • Title: ➤  Directional stability in flight with bank angle constraint as a condition defining a minimum acceptable value for n[superscript v]
            • Author:
            • Language: English
            • Number of Pages: Median: 13
            • Publisher: H.M.S.O.
            • Publish Date:
            • Publish Location: London

            “Directional stability in flight with bank angle constraint as a condition defining a minimum acceptable value for n[superscript v]” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

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

            Online Marketplaces

            Find Directional stability in flight with bank angle constraint as a condition defining a minimum acceptable value for n[superscript v] at online marketplaces:


            13A form of lateral instability of lifting free-flight models towed by a helicopter

            By

            “A form of lateral instability of lifting free-flight models towed by a helicopter” Metadata:

            • Title: ➤  A form of lateral instability of lifting free-flight models towed by a helicopter
            • Author:
            • Language: English
            • Number of Pages: Median: 15
            • Publisher: H.M. Stationery Off.
            • Publish Date:
            • Publish Location: London

            “A form of lateral instability of lifting free-flight models towed by a helicopter” 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

            Online Marketplaces

            Find A form of lateral instability of lifting free-flight models towed by a helicopter at online marketplaces:


            14Maximum likelihood method for estimating airplane stability and control parameters from flight data in frequency domain

            By

            “Maximum likelihood method for estimating airplane stability and control parameters from flight data in frequency domain” Metadata:

            • Title: ➤  Maximum likelihood method for estimating airplane stability and control parameters from flight data in frequency domain
            • Author:
            • Language: English
            • Number of Pages: Median: 57
            • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office - For sale by the National Technical Information Service]
            • Publish Date:
            • Publish Location: ➤  Washington, D.C - [Springfield, Va

            “Maximum likelihood method for estimating airplane stability and control parameters from flight data in frequency domain” 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

            Online Marketplaces

            Find Maximum likelihood method for estimating airplane stability and control parameters from flight data in frequency domain at online marketplaces:


            15Theroetical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack

            By

            “Theroetical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack” Metadata:

            • Title: ➤  Theroetical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack
            • Author:
            • Language: English
            • Number of Pages: Median: 96
            • Publisher: ➤  National Aeronautics and Space Administration - for sale by the National Technical Information Office
            • Publish Date:
            • Publish Location: Washington - Springfield, Va

            “Theroetical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack” 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

            Online Marketplaces

            Find Theroetical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack at online marketplaces:


            16The interference of the model support mast with measurements of the longitudinal and lateral aerodynamic coefficients

            By

            “The interference of the model support mast with measurements of the longitudinal and lateral aerodynamic coefficients” Metadata:

            • Title: ➤  The interference of the model support mast with measurements of the longitudinal and lateral aerodynamic coefficients
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration
            • Publish Date:
            • Publish Location: Washington, DC

            “The interference of the model support mast with measurements of the longitudinal and lateral aerodynamic coefficients” 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.

            Online Borrowing:

              Online Marketplaces

              Find The interference of the model support mast with measurements of the longitudinal and lateral aerodynamic coefficients at online marketplaces:


              17Capturing and tracking performance of the horizontal guidance and control systems of the terminal configured vehicle

              By

              “Capturing and tracking performance of the horizontal guidance and control systems of the terminal configured vehicle” Metadata:

              • Title: ➤  Capturing and tracking performance of the horizontal guidance and control systems of the terminal configured vehicle
              • Author:
              • Language: English
              • Number of Pages: Median: 30
              • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
              • Publish Date:
              • Publish Location: ➤  Washington, D.C - [Springfield, Va

              “Capturing and tracking performance of the horizontal guidance and control systems of the terminal configured vehicle” 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

              Online Marketplaces

              Find Capturing and tracking performance of the horizontal guidance and control systems of the terminal configured vehicle at online marketplaces:


              18Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds

              By

              “Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds” Metadata:

              • Title: ➤  Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds
              • Author:
              • Language: English
              • Number of Pages: Median: 197
              • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
              • Publish Date:
              • Publish Location: ➤  Washington, D.C - [Springfield, Va

              “Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds” 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

              Online Marketplaces

              Find Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds at online marketplaces:


              19Recent progress towards predicting aircraft ground handling performance

              By

              “Recent progress towards predicting aircraft ground handling performance” Metadata:

              • Title: ➤  Recent progress towards predicting aircraft ground handling performance
              • Author:
              • Language: English
              • Number of Pages: Median: 29
              • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
              • Publish Date:
              • Publish Location: ➤  Washington, D.C - [Springfield, Va

              “Recent progress towards predicting aircraft ground handling performance” 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

              Online Marketplaces

              Find Recent progress towards predicting aircraft ground handling performance at online marketplaces:


              20Relative control effectiveness technique with application to airplane control coordination

              By

              “Relative control effectiveness technique with application to airplane control coordination” Metadata:

              • Title: ➤  Relative control effectiveness technique with application to airplane control coordination
              • Author:
              • Language: English
              • Publisher: ➤  For sale by the National Technical Information Service,] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
              • Publish Date:
              • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

              “Relative control effectiveness technique with application to airplane control coordination” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

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

              Online Access

              Downloads Are Not Available:

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

              Online Borrowing:

                Online Marketplaces

                Find Relative control effectiveness technique with application to airplane control coordination at online marketplaces:


                21Lateral stability analysis for X-29A drop model using system identification methodology

                By

                “Lateral stability analysis for X-29A drop model using system identification methodology” Metadata:

                • Title: ➤  Lateral stability analysis for X-29A drop model using system identification methodology
                • Author:
                • Language: English
                • Number of Pages: Median: 24
                • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
                • Publish Date:
                • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                “Lateral stability analysis for X-29A drop model using system identification methodology” 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.

                Online Borrowing:

                  Online Marketplaces

                  Find Lateral stability analysis for X-29A drop model using system identification methodology at online marketplaces:


                  22Thrust vectoring for lateral-directional stability

                  By

                  “Thrust vectoring for lateral-directional stability” Metadata:

                  • Title: ➤  Thrust vectoring for lateral-directional stability
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Technical Information Service, distributor] - National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
                  • Publish Date:
                  • Publish Location: ➤  [Springfield, Va - Edwards, Calif

                  “Thrust vectoring for lateral-directional stability” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

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

                  Online Access

                  Downloads Are Not Available:

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

                  Online Borrowing:

                    Online Marketplaces

                    Find Thrust vectoring for lateral-directional stability at online marketplaces:


                    23Simulator evaluation of separation of display parameters in path-following tasks

                    By

                    “Simulator evaluation of separation of display parameters in path-following tasks” Metadata:

                    • Title: ➤  Simulator evaluation of separation of display parameters in path-following tasks
                    • Author:
                    • Language: English
                    • Number of Pages: Median: 41
                    • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
                    • Publish Date:
                    • Publish Location: ➤  Washington, D.C - [Springfield, Va

                    “Simulator evaluation of separation of display parameters in path-following tasks” 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

                    Online Marketplaces

                    Find Simulator evaluation of separation of display parameters in path-following tasks at online marketplaces:


                    24The application of parameter estimation to flight measurements to obtain lateral-directional stability derivatives of an augmented jet-flap STOL airplane

                    By

                    “The application of parameter estimation to flight measurements to obtain lateral-directional stability derivatives of an augmented jet-flap STOL airplane” Metadata:

                    • Title: ➤  The application of parameter estimation to flight measurements to obtain lateral-directional stability derivatives of an augmented jet-flap STOL airplane
                    • Author:
                    • Language: English
                    • Number of Pages: Median: 56
                    • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
                    • Publish Date:
                    • Publish Location: ➤  Washington, D.C - [Springfield, Va

                    “The application of parameter estimation to flight measurements to obtain lateral-directional stability derivatives of an augmented jet-flap STOL airplane” 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

                    Online Marketplaces

                    Find The application of parameter estimation to flight measurements to obtain lateral-directional stability derivatives of an augmented jet-flap STOL airplane at online marketplaces:


                    25Lateral and longitudinal stability and control parameters for the space shuttle Discovery as determined from flight test data

                    By

                    “Lateral and longitudinal stability and control parameters for the space shuttle Discovery as determined from flight test data” Metadata:

                    • Title: ➤  Lateral and longitudinal stability and control parameters for the space shuttle Discovery as determined from flight test data
                    • Author:
                    • Language: English
                    • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
                    • Publish Date:
                    • Publish Location: [Springfield, Va - Hampton, Va

                    “Lateral and longitudinal stability and control parameters for the space shuttle Discovery as determined from flight test data” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 1988
                    • Is Full Text Available: No
                    • Is The Book Public: No
                    • Access Status: No_ebook

                    Online Access

                    Downloads Are Not Available:

                    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.

                    Online Borrowing:

                      Online Marketplaces

                      Find Lateral and longitudinal stability and control parameters for the space shuttle Discovery as determined from flight test data at online marketplaces:


                      26Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data

                      By

                      “Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data” Metadata:

                      • Title: ➤  Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
                      • Publish Date:
                      • Publish Location: Hampton, Va

                      “Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test 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

                      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.

                      Online Borrowing:

                        Online Marketplaces

                        Find Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data at online marketplaces:


                        27Prediction of motions of an airplane resulting from abrupt movement of lateral or directional controls

                        By

                        “Prediction of motions of an airplane resulting from abrupt movement of lateral or directional controls” Metadata:

                        • Title: ➤  Prediction of motions of an airplane resulting from abrupt movement of lateral or directional controls
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 20
                        • Publisher: NACA
                        • Publish Date:
                        • Publish Location: Washington

                        “Prediction of motions of an airplane resulting from abrupt movement of lateral or directional controls” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1945
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

                        Online Marketplaces

                        Find Prediction of motions of an airplane resulting from abrupt movement of lateral or directional controls at online marketplaces:


                        28Low-speed wind-tunnel measurements of the oscillatory lateral stability derivatives for a model of a slender aircraft (HP 115) including the effects of frequency parameter

                        By

                        “Low-speed wind-tunnel measurements of the oscillatory lateral stability derivatives for a model of a slender aircraft (HP 115) including the effects of frequency parameter” Metadata:

                        • Title: ➤  Low-speed wind-tunnel measurements of the oscillatory lateral stability derivatives for a model of a slender aircraft (HP 115) including the effects of frequency parameter
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 30
                        • Publisher: H.M. Stationery Off.
                        • Publish Date:
                        • Publish Location: London

                        “Low-speed wind-tunnel measurements of the oscillatory lateral stability derivatives for a model of a slender aircraft (HP 115) including the effects of frequency parameter” 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

                        Online Marketplaces

                        Find Low-speed wind-tunnel measurements of the oscillatory lateral stability derivatives for a model of a slender aircraft (HP 115) including the effects of frequency parameter at online marketplaces:


                        29Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model

                        By

                        “Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model” Metadata:

                        • Title: ➤  Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 22
                        • Publisher: H.M.S.O.
                        • Publish Date:
                        • Publish Location: London

                        “Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model” Subjects and Themes:

                        Edition Identifiers:

                        • The Open Library ID: OL5586072M
                        • Online Computer Library Center (OCLC) ID: 6163138
                        • Library of Congress Control Number (LCCN): 67104629

                        Access and General Info:

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

                        Online Marketplaces

                        Find Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model at online marketplaces:


                        30Turbulence and lateral-directional flying qualities

                        By

                        “Turbulence and lateral-directional flying qualities” Metadata:

                        • Title: ➤  Turbulence and lateral-directional flying qualities
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 260
                        • Publisher: ➤  For sale by the National Technical Information Service
                        • Publish Date:
                        • Publish Location: ➤  [Washington - Springfield, Va.]

                        “Turbulence and lateral-directional flying qualities” 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 Turbulence and lateral-directional flying qualities at online marketplaces:


                        31Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivatives

                        By

                        “Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivatives” Metadata:

                        • Title: ➤  Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivatives
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 83
                        • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - Available from National Technical Information Service
                        • Publish Date:
                        • Publish Location: ➤  Edwards, Calif - Springfield, Va

                        “Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivatives” 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 Marketplaces

                        Find Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivatives at online marketplaces:


                        32A theoretical analysis of the dynamic lateral stability and control of a parawing vehicle

                        By

                        “A theoretical analysis of the dynamic lateral stability and control of a parawing vehicle” Metadata:

                        • Title: ➤  A theoretical analysis of the dynamic lateral stability and control of a parawing vehicle
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 45
                        • Publisher: ➤  National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.
                        • Publish Date:
                        • Publish Location: [Washington]

                        “A theoretical analysis of the dynamic lateral stability and control of a parawing vehicle” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

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

                        Online Marketplaces

                        Find A theoretical analysis of the dynamic lateral stability and control of a parawing vehicle at online marketplaces:


                        Top of Page