A modeling methodology and flight simulations are presented that account for the external loads of a slender high-speed vehicle maneuvering with divert and attitude control jets. The slender vehicle structure leads to a deformable vehicle and a coupled fluid–structure interaction. The jets apply a force to the vehicle via thrust, but the exhaust interacts with the free-stream flow that may change the applied load and control effectiveness. The resulting fluid–structure–jet interaction problem is considered and a reduced modeling method has been developed to enable vehicle flight simulation with the coupled aeroelastic and flight mechanics equations. The reduced model is based on the high-fidelity steady-state computational fluid dynamics solutions of the fluid–structure–jet interaction problem and incorporated into a flight simulation framework. The simulation results highlight the effects of considering jet interaction and fluid–structure–jet interaction on vehicle maneuverability and agility.


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    Titel :

    Fluid–Structure–Jet Interaction Modeling and Simulation of High-Speed Vehicles


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    2017-09-13


    Format / Umfang :

    12 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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