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11999 NASA High-Speed Research Program Aerodynamic Performance Workshop

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“1999 NASA High-Speed Research Program Aerodynamic Performance Workshop” Metadata:

  • Title: ➤  1999 NASA High-Speed Research Program Aerodynamic Performance Workshop
  • Author: ➤  
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
  • Publish Date:
  • Publish Location: Hampton, Va - [Springfield, Va

“1999 NASA High-Speed Research Program Aerodynamic Performance Workshop” 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

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    2Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept

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    “Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept” Metadata:

    • Title: ➤  Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
    • Author:
    • Language: English
    • Number of Pages: Median: 23
    • Publisher: ➤  Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - Springfield, VA - Hampton, Va

    “Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept” 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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      3Euler/Navier-Stokes flow computations on flexible configurations for stability analysis

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      “Euler/Navier-Stokes flow computations on flexible configurations for stability analysis” Metadata:

      • Title: ➤  Euler/Navier-Stokes flow computations on flexible configurations for stability analysis
      • Author:
      • Language: English
      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, American Institute of Aeronautics and Astronautics
      • Publish Date:
      • Publish Location: ➤  Springfield, Va - [Washington, D.C

      “Euler/Navier-Stokes flow computations on flexible configurations for stability analysis” 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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        4Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊

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        “Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Metadata:

        • Title: ➤  Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
        • Author:
        • Language: English
        • Number of Pages: Median: 145
        • Publisher: ➤  National Aeronautics and Space Administration - Langley Research Center - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  Hampton, Va - [Washington, DC - Springfield, Va

        “Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

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

        Online Access

        Downloads Are Not Available:

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          5Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel

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          “Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel” Metadata:

          • Title: ➤  Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel
          • 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

          “Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel” 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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            6The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge

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            “The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge” Metadata:

            • Title: ➤  The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge
            • Author:
            • Language: English
            • Publisher: ➤  Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
            • Publish Date:
            • Publish Location: [Springfield, Va - Hampton, VA

            “The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge” 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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              7Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops

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              “Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops” Metadata:

              • Title: ➤  Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops
              • Author:
              • Language: English
              • Number of Pages: Median: 63
              • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center - For sale by the National Technical Information Service
              • Publish Date:
              • Publish Location: ➤  Springfield, Va - Hampton, Va - [Washington, D.C.]

              “Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops” 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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                8Performance of a low-power subsonic-arc-attachment arcjet thruster

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                “Performance of a low-power subsonic-arc-attachment arcjet thruster” Metadata:

                • Title: ➤  Performance of a low-power subsonic-arc-attachment arcjet thruster
                • Author:
                • Language: English
                • Publisher: ➤  National Technical Information Service, distributor - NASA
                • Publish Date:
                • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                “Performance of a low-power subsonic-arc-attachment arcjet thruster” 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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                  9Full-scale hingeless rotor performance and loads

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                  “Full-scale hingeless rotor performance and loads” Metadata:

                  • Title: ➤  Full-scale hingeless rotor performance and loads
                  • 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

                  “Full-scale hingeless rotor performance and loads” 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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                    10Low-speed wind tunnel tests of two waverider configuration models

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                    “Low-speed wind tunnel tests of two waverider configuration models” Metadata:

                    • Title: ➤  Low-speed wind tunnel tests of two waverider configuration models
                    • Author:
                    • Language: English
                    • Publisher: ➤  [National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor
                    • Publish Date:
                    • Publish Location: ➤  Washington, D.C - Springfield, Va

                    “Low-speed wind tunnel tests of two waverider configuration models” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

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

                    Online Access

                    Downloads Are Not Available:

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                      11Nonlinear stability of supersonic jets

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                      “Nonlinear stability of supersonic jets” Metadata:

                      • Title: ➤  Nonlinear stability of supersonic jets
                      • Author:
                      • Language: English
                      • Publisher: ➤  NASA Langley Research Center - Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University - National Technical Information Service, distributor - National Aeronautics and Space Administration
                      • Publish Date:
                      • Publish Location: ➤  Springfield, Va - Norfolk, Va - Hampton, Va - [Springfield, Va - [Washington, DC

                      “Nonlinear stability of supersonic jets” 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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                        12Aeroelastic stability of a full-scale hingeless rotor

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                        “Aeroelastic stability of a full-scale hingeless rotor” Metadata:

                        • Title: ➤  Aeroelastic stability of a full-scale hingeless rotor
                        • 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

                        “Aeroelastic stability of a full-scale hingeless rotor” 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:

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                          13A spectrally accurate boundary-layer code for infinite swept wings

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                          “A spectrally accurate boundary-layer code for infinite swept wings” Metadata:

                          • Title: ➤  A spectrally accurate boundary-layer code for infinite swept wings
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                          • Publish Date:
                          • Publish Location: Hampton, Va - [Springfield, Va

                          “A spectrally accurate boundary-layer code for infinite swept wings” 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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                          Downloads Are Not Available:

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                            14Aerothermodynamics of the Mars Global Surveyor spacecraft

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                            “Aerothermodynamics of the Mars Global Surveyor spacecraft” Metadata:

                            • Title: ➤  Aerothermodynamics of the Mars Global Surveyor spacecraft
                            • Author:
                            • Language: English
                            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
                            • Publish Date:
                            • Publish Location: Hampton, Va - [Springfield, Va

                            “Aerothermodynamics of the Mars Global Surveyor spacecraft” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1998
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

                            Online Access

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                              15FPCAS3D user's guide

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                              “FPCAS3D user's guide” Metadata:

                              • Title: FPCAS3D user's guide
                              • Author:
                              • Language: English
                              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                              • Publish Date:
                              • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                              “FPCAS3D user's guide” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

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

                              Online Access

                              Downloads Are Not Available:

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

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                                16Modeling of longitudinal unsteady aerodynamics of a wing-tail combination

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                                “Modeling of longitudinal unsteady aerodynamics of a wing-tail combination” Metadata:

                                • Title: ➤  Modeling of longitudinal unsteady aerodynamics of a wing-tail combination
                                • Author:
                                • Language: English
                                • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                                • Publish Date:
                                • Publish Location: Hampton, Va - [Springfield, Va

                                “Modeling of longitudinal unsteady aerodynamics of a wing-tail combination” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

                                • First Year Published: 1999
                                • Is Full Text Available: No
                                • Is The Book Public: No
                                • Access Status: No_ebook

                                Online Access

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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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                                  17Direct adaptive aircraft control using dynamic cell structure neural networks

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                                  “Direct adaptive aircraft control using dynamic cell structure neural networks” Metadata:

                                  • Title: ➤  Direct adaptive aircraft control using dynamic cell structure neural networks
                                  • Author:
                                  • Language: English
                                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
                                  • Publish Date:
                                  • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                                  “Direct adaptive aircraft control using dynamic cell structure neural networks” Subjects and Themes:

                                  Edition Identifiers:

                                  Access and General Info:

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

                                  Online Access

                                  Downloads Are Not Available:

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

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                                    18Determination of stability and control derivatives for the NASA F/A-18 HARV from flight data using the maximum likelihood method

                                    By

                                    “Determination of stability and control derivatives for the NASA F/A-18 HARV from flight data using the maximum likelihood method” Metadata:

                                    • Title: ➤  Determination of stability and control derivatives for the NASA F/A-18 HARV from flight data using the maximum likelihood method
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - West Virginia University
                                    • Publish Date:
                                    • Publish Location: ➤  Morgantown, WV - [Washington, DC - Springfield, Va

                                    “Determination of stability and control derivatives for the NASA F/A-18 HARV from flight data using the maximum likelihood method” Subjects and Themes:

                                    Edition Identifiers:

                                    Access and General Info:

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

                                    Online Access

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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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                                      19Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients

                                      By

                                      “Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients” Metadata:

                                      • Title: ➤  Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients
                                      • Author:
                                      • Language: English
                                      • Number of Pages: Median: 98
                                      • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office
                                      • Publish Date:
                                      • Publish Location: Washington, D.C

                                      “Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients” 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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                                      20Identification of dynamic systems - applications to aircraft

                                      By

                                      “Identification of dynamic systems - applications to aircraft” Metadata:

                                      • Title: ➤  Identification of dynamic systems - applications to aircraft
                                      • Author:
                                      • Publisher: AGARD
                                      • Publish Date:
                                      • Publish Location: Neuilly sur Seine, France

                                      “Identification of dynamic systems - applications to aircraft” 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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                                      21Static aeroelasticity in combat aircraft

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                                      “Static aeroelasticity in combat aircraft” Metadata:

                                      • Title: ➤  Static aeroelasticity in combat aircraft
                                      • Author: ➤  
                                      • Publisher: AGARD
                                      • Publish Date:
                                      • Publish Location: Neuilly sur Seine, France

                                      “Static aeroelasticity in combat aircraft” 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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                                      22CLMNANAL, a C++ program for application of the Coleman stability analysis to rotorcraft

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                                      “CLMNANAL, a C++ program for application of the Coleman stability analysis to rotorcraft” Metadata:

                                      • Title: ➤  CLMNANAL, a C++ program for application of the Coleman stability analysis to rotorcraft
                                      • Author:
                                      • Language: English
                                      • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                                      • Publish Date:
                                      • Publish Location: Hampton, Va - [Springfield, Va

                                      “CLMNANAL, a C++ program for application of the Coleman stability analysis to rotorcraft” Subjects and Themes:

                                      Edition Identifiers:

                                      Access and General Info:

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

                                      Online Access

                                      Downloads Are Not Available:

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

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                                        23Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight

                                        By

                                        “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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                                          24Effect of control surface mass unbalance on the stability of a closed-loop active control system

                                          By

                                          “Effect of control surface mass unbalance on the stability of a closed-loop active control system” Metadata:

                                          • Title: ➤  Effect of control surface mass unbalance on the stability of a closed-loop active control system
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - National Technical Information Service, distributor]
                                          • Publish Date:
                                          • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                          “Effect of control surface mass unbalance on the stability of a closed-loop active control system” Subjects and Themes:

                                          Edition Identifiers:

                                          Access and General Info:

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

                                          Online Access

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                                            25Analysis of flight data from a high-incidence research model by system identification methods

                                            By

                                            “Analysis of flight data from a high-incidence research model by system identification methods” Metadata:

                                            • Title: ➤  Analysis of flight data from a high-incidence research model by system identification methods
                                            • Author:
                                            • Language: English
                                            • Publisher: ➤  National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
                                            • Publish Date:
                                            • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                            “Analysis of flight data from a high-incidence research model by system identification methods” 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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                                              26Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept

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                                              • Title: ➤  Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept
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                                              • Language: English
                                              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Marshall Space Flight Center
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                                              • Publish Location: [Springfield, Va - MSFC, Ala

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                                              • First Year Published: 1995
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                                                27Subsonic wing optimization for handling qualities using ACSYNT

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                                                • Title: ➤  Subsonic wing optimization for handling qualities using ACSYNT
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                                                • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
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                                                • Publish Location: ➤  [Washington, DC - Springfield, Va

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                                                • First Year Published: 1996
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                                                  28Euler technology assessment

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                                                  • Title: Euler technology assessment
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                                                  • Publish Location: Hampton, Va - Springfield, VA

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                                                  • First Year Published: 1998
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                                                    29Theory of aerodynamic instability and the mechanism of flutter

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                                                    • Number of Pages: Median: 23
                                                    • Publisher: NACA
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                                                    • Publish Location: Washington

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                                                    • First Year Published: 1935
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                                                      30Rotorcraft dynamics 1984

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                                                      • Title: Rotorcraft dynamics 1984
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                                                      • Language: English
                                                      • Number of Pages: Median: 501
                                                      • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service
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                                                      • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

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                                                      • First Year Published: 1985
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                                                        31The application of linear maximum likelihood estimation of aerodynamic derivatives for the Bell-205 and Bell-206

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                                                        • Title: ➤  The application of linear maximum likelihood estimation of aerodynamic derivatives for the Bell-205 and Bell-206
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                                                        • Number of Pages: Median: 54
                                                        • Publisher: ➤  National Research Council Canada
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                                                        • Publish Location: Ottawa

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                                                        • First Year Published: 1987
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                                                        32Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft

                                                        “Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft” Metadata:

                                                        • Title: ➤  Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
                                                        • Language: English
                                                        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
                                                        • Publish Date:
                                                        • Publish Location: ➤  Edwards, Calif - Springfield, VA

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                                                        • First Year Published: 1999
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                                                          33Design of robust suboptimal controllers for a generalized quadratic criterion

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                                                          • Title: ➤  Design of robust suboptimal controllers for a generalized quadratic criterion
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                                                          • Language: English
                                                          • Number of Pages: Median: 57
                                                          • Publisher: ➤  Naval Postgraduate School - Available from National Technical Information Service
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                                                          • Publish Location: ➤  Monterey, Calif - Springfield, Va

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                                                          • First Year Published: 1992
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                                                            Wiki

                                                            Source: Wikipedia

                                                            Wikipedia Results

                                                            Search Results from Wikipedia

                                                            Atmospheric entry

                                                            half-angle and properly placed center of mass, a sphere-cone can provide aerodynamic stability from Keplerian entry to surface impact. (The half-angle is the angle

                                                            Rifling

                                                            firearms's barrel for imparting a spin to a projectile to improve its aerodynamic stability and accuracy. It is also the term (as a verb) for creating such

                                                            Relaxed stability

                                                            aircraft is said to have relaxed stability if it has low or negative stability. An aircraft with negative stability will have a tendency to change its

                                                            Aerodynamics

                                                            eighteenth century, although observations of fundamental concepts such as aerodynamic drag were recorded much earlier. Most of the early efforts in aerodynamics

                                                            Aircraft flight dynamics

                                                            physical situation and is called Prandtl–Glauert singularity. see Aerodynamic force Stability is the ability of the aircraft to counteract disturbances to

                                                            Structural integrity and failure

                                                            (2001). In the Wake of Tacoma: Suspension Bridges and the Quest for Aerodynamic Stability. ASCE Publications. p. 139. ISBN 0-7844-0542-5. K. Billah and R

                                                            Wing configuration

                                                            are the low wing loading and high wetted area needed to obtain aerodynamic stability. Variants are: Tailless delta: a classic high-speed design, used

                                                            BASE jumping

                                                            at lower speeds, have less aerodynamic control. The attitude of the body at the moment of jumping determines the stability of flight in the first few

                                                            Strait of Messina Bridge

                                                            Structurae. The greatest problem in designing the bridge is the aerodynamic stability of the deck under wind as well as seismic activity. Sabelli, Chiara

                                                            Chord (aeronautics)

                                                            various wing shapes, the mean aerodynamic chord (abbreviated MAC) is used, although it is complex to calculate. The mean aerodynamic chord is used for calculating