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- W2123268986 abstract "The possibility of use of energy supply as the method of the overall control of the airflow is defined in the experimental and theoretical research (Adegren et al., 2001, 2005; Bazyma & Rashkovan, 2005; Tret’yakov et al., 1994, 1996). As an example, reduction of head resistance of a supersonic aircraft can be achieved with the introduction of energy into the contrary incoming flow. On the other hand, supply of energy may be used to minimize negative consequences of the shock-wave interaction when the streamlining of the aerodynamic configurations of the compound form occurs. For example, oblique shock waves, which are distributed from the bow part of an airplane or a rocket, can interact with a bow shock wave of any part of the fuselage construction (tail unit, suspension, hood, diffuser, etc.). In certain cases the shock-wave interaction can result in significant negative and even catastrophic consequences for the aircraft." @default.
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- W2123268986 date "2012-03-23" @default.
- W2123268986 modified "2023-10-02" @default.
- W2123268986 title "Numerical Simulation of the Unsteady Shock Interaction of Blunt Body Flows" @default.
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- W2123268986 doi "https://doi.org/10.5772/36144" @default.
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