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      Unsteady Side Loads in a Thrust-Optimized Contour Nozzle at Hysteresis Regime

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      AIAA Journal
      American Institute of Aeronautics and Astronautics (AIAA)

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          Magnus Effect over Finned Projectiles

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            Restricted Shock Separation in Rocket Nozzles

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              Sea level side loads in high-area-ratio rocket engines

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                Author and article information

                Journal
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics (AIAA)
                0001-1452
                1533-385X
                September 2004
                September 2004
                : 42
                : 9
                : 1878-1888
                Article
                10.2514/1.2425
                c98fe7f8-86e8-4478-81a2-ff49577dfad9
                © 2004
                History

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