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1High angle of attack aerodynamics

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Book's cover

“High angle of attack aerodynamics” Metadata:

  • Title: ➤  High angle of attack aerodynamics
  • Author:
  • Language: English
  • Number of Pages: Median: 399
  • Publisher: Springer - Springer-Verlag
  • Publish Date:
  • Publish Location: New York

“High angle of attack aerodynamics” Subjects and Themes:

Edition Identifiers:

Access and General Info:

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

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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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2Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack

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“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.

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    3X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data

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    “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.

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      4Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring

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      “Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring” Metadata:

      • Title: ➤  Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
      • Author:
      • Language: English
      • Number of Pages: Median: 65
      • Publisher: ➤  National Technical Information Service, distributor - NASA, Dryden Flight Research Center - National Aeronautics and Space Administration, Dryden Flight Research Center - Available from National Technical Information Service
      • Publish Date:
      • Publish Location: ➤  Edwards, Calif - Springfield, Va - [Springfield, Va

      “Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring” 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:

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        5Supersonic flow around circular cones at angles of attack

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        “Supersonic flow around circular cones at angles of attack” Metadata:

        • Title: ➤  Supersonic flow around circular cones at angles of attack
        • Author:
        • Language: English
        • Number of Pages: Median: 11
        • Publisher: U.S. Govt. Print. Off.
        • Publish Date:
        • Publish Location: Washington

        “Supersonic flow around circular cones at angles of attack” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1951
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

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        6Tables for supersonic flow of helium around right circular cones at zero angle of attack

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        “Tables for supersonic flow of helium around right circular cones at zero angle of attack” Metadata:

        • Title: ➤  Tables for supersonic flow of helium around right circular cones at zero angle of attack
        • Author:
        • Language: English
        • Number of Pages: Median: 24
        • Publisher: ➤  Scientific and Technical Information Office, National Aeronautics and Space Administration; [for sale by the Supt. of Docs., U.S. Govt. Print. Off.]
        • Publish Date:
        • Publish Location: Washington

        “Tables for supersonic flow of helium around right circular cones at zero angle of attack” 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

        Online Marketplaces

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        7Experimetal investigations on wing-body combinations and their components at high angles of attack in the subsonic and transonic speed range

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        “Experimetal investigations on wing-body combinations and their components at high angles of attack in the subsonic and transonic speed range” Metadata:

        • Title: ➤  Experimetal investigations on wing-body combinations and their components at high angles of attack in the subsonic and transonic speed range
        • Author:
        • Language: English
        • Number of Pages: Median: 83
        • Publisher: ➤  Deutsche Forschungsanstalt für Luft- und Raumfahrt
        • Publish Date:
        • Publish Location: Köln

        “Experimetal investigations on wing-body combinations and their components at high angles of attack in the subsonic and transonic speed range” 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 Marketplaces

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        8Nose up

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        “Nose up” Metadata:

        • Title: Nose up
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, NASA History Office
        • Publish Date:
        • Publish Location: Washington, D.C

        “Nose up” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 2004
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

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        9Reduzierung der thermischen Belastung eines Hyperschallflugzeugs durch optimale Bahnsteuerung

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        “Reduzierung der thermischen Belastung eines Hyperschallflugzeugs durch optimale Bahnsteuerung” Metadata:

        • Title: ➤  Reduzierung der thermischen Belastung eines Hyperschallflugzeugs durch optimale Bahnsteuerung
        • Author:
        • Language: ger
        • Number of Pages: Median: 100
        • Publisher: Utz, Wissenschaft
        • Publish Date:
        • Publish Location: München

        “Reduzierung der thermischen Belastung eines Hyperschallflugzeugs durch optimale Bahnsteuerung” 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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        10Fluid dynamics of high angle of attack

        “Fluid dynamics of high angle of attack” Metadata:

        • Title: ➤  Fluid dynamics of high angle of attack
        • Language: English
        • Number of Pages: Median: 439
        • Publisher: Springer-Verlag
        • Publish Date:
        • Publish Location: New York - Berlin

        “Fluid dynamics of high angle of attack” 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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        11Preliminary results from an airdata enhancement algorithm with application to high-angle-of-attack flights

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        “Preliminary results from an airdata enhancement algorithm with application to high-angle-of-attack flights” Metadata:

        • Title: ➤  Preliminary results from an airdata enhancement algorithm with application to high-angle-of-attack flights
        • Author:
        • Language: English
        • Number of Pages: Median: 41
        • Publisher: ➤  National Aeronautics and Space Administration, Ames Resarch Center, Dryden Flight Research Facility - For sale by the National Technical Information Service]
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - Edwards, Calif

        “Preliminary results from an airdata enhancement algorithm with application to high-angle-of-attack flights” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

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

        Online Access

        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:

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          12A numerical analysis applied to high angle of attack three-dimensional inlets

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          “A numerical analysis applied to high angle of attack three-dimensional inlets” Metadata:

          • Title: ➤  A numerical analysis applied to high angle of attack three-dimensional inlets
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
          • Publish Date:
          • Publish Location: [Cleveland, Ohio

          “A numerical analysis applied to high angle of attack three-dimensional inlets” 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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            13Problems of aircraft behaviour at high angles of attack

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            “Problems of aircraft behaviour at high angles of attack” Metadata:

            • Title: ➤  Problems of aircraft behaviour at high angles of attack
            • Author:
            • Language: English
            • Number of Pages: Median: 110
            • Publisher: ➤  North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development
            • Publish Date:
            • Publish Location: [Paris]

            “Problems of aircraft behaviour at high angles of attack” 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

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            14A study of the effects of jets injected from a slender body of revolution on the side forces, acting on it at large angles of attack in low speeds

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            “A study of the effects of jets injected from a slender body of revolution on the side forces, acting on it at large angles of attack in low speeds” Metadata:

            • Title: ➤  A study of the effects of jets injected from a slender body of revolution on the side forces, acting on it at large angles of attack in low speeds
            • Author:
            • Language: English
            • Number of Pages: Median: 27
            • Publisher: ➤  Dept. of Aeronautical Engineering, Technion, Israel Institute of Technology
            • Publish Date:
            • Publish Location: Haifa

            “A study of the effects of jets injected from a slender body of revolution on the side forces, acting on it at large angles of attack in low speeds” 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

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            15Normal- and oblique-shock flow parameters in equilibrium air

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            “Normal- and oblique-shock flow parameters in equilibrium air” Metadata:

            • Title: ➤  Normal- and oblique-shock flow parameters in equilibrium air
            • Author:
            • Language: English
            • Number of Pages: Median: 154
            • Publisher: ➤  Scientific and Technical Information Office, National Aeronautics and Space Administration - for sale by the National Technical Information Service
            • Publish Date:
            • Publish Location: Springfield, Va - Washington

            “Normal- and oblique-shock flow parameters in equilibrium air” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1975
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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            16Normal- and oblique-shock flow parameters in equilibrium air including attached-shock solutions for surfaces at angles of attack, sweep, and dihedral

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            “Normal- and oblique-shock flow parameters in equilibrium air including attached-shock solutions for surfaces at angles of attack, sweep, and dihedral” Metadata:

            • Title: ➤  Normal- and oblique-shock flow parameters in equilibrium air including attached-shock solutions for surfaces at angles of attack, sweep, and dihedral
            • Author:
            • Language: English
            • Number of Pages: Median: 154
            • Publisher: ➤  For sale by the National Technical Information Service - Scientific and Technical Information Office, National Aeronautics and Space Administration
            • Publish Date:
            • Publish Location: Springfield, Va - Washington

            “Normal- and oblique-shock flow parameters in equilibrium air including attached-shock solutions for surfaces at angles of attack, sweep, and dihedral” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1975
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

            Online Marketplaces

            Find Normal- and oblique-shock flow parameters in equilibrium air including attached-shock solutions for surfaces at angles of attack, sweep, and dihedral at online marketplaces:


            17The sail at small angle of incidence at supersonic, hypersonic and sonic speed

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            “The sail at small angle of incidence at supersonic, hypersonic and sonic speed” Metadata:

            • Title: ➤  The sail at small angle of incidence at supersonic, hypersonic and sonic speed
            • Author:
            • Language: English
            • Number of Pages: Median: 21
            • Publisher: Ministry of Technology
            • Publish Date:
            • Publish Location: Farnborough [Eng.]

            “The sail at small angle of incidence at supersonic, hypersonic and sonic speed” 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

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            18Measurements of drag, base pressure and base aerodynamic heat transfer appropriate to 8.5⁰ semi-angle sharp cones in free flight at mach numbers from 0.8 to 3.8

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            “Measurements of drag, base pressure and base aerodynamic heat transfer appropriate to 8.5⁰ semi-angle sharp cones in free flight at mach numbers from 0.8 to 3.8” Metadata:

            • Title: ➤  Measurements of drag, base pressure and base aerodynamic heat transfer appropriate to 8.5⁰ semi-angle sharp cones in free flight at mach numbers from 0.8 to 3.8
            • Author:
            • Language: English
            • Number of Pages: Median: 19
            • Publisher: H.M.S.O.
            • Publish Date:
            • Publish Location: London

            “Measurements of drag, base pressure and base aerodynamic heat transfer appropriate to 8.5⁰ semi-angle sharp cones in free flight at mach numbers from 0.8 to 3.8” 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

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            19Flight-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

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            “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

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