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      Calculation of plane steady transonic flows

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      AIAA Journal
      American Institute of Aeronautics and Astronautics (AIAA)

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          Drag of a Finite Wedge at High Subsonic Speeds

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            The Flow over a Wedge Profile at Mach Number 1

            (1950)
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              Expansion procedures and similarity laws for transonic flow

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                Author and article information

                Journal
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics (AIAA)
                0001-1452
                1533-385X
                January 1971
                January 1971
                : 9
                : 1
                : 114-121
                Article
                10.2514/3.6131
                2d9567a3-a138-4f27-832b-a856bdf8445b
                © 1971
                History

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