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    Fluidic Thrust Vector Control of Aerospace Vehicles: State-of-the-Art Review and Future Prospects

    Source: Journal of Fluids Engineering:;2023:;volume( 145 ):;issue: 008::page 80801-1
    Author:
    Das, Arnab K.
    ,
    Acharyya, Kaustubh
    ,
    Mankodi, Tapan K.
    ,
    Saha, Ujjwal K.
    DOI: 10.1115/1.4062109
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An efficient propulsion system holds the key to the smooth operation of any aerospace vehicle over different flight regimes. Apart from generating the necessary thrust, emphasis has also been laid on vectoring the direction of thrust. The primitive modes of thrust vectoring chiefly focused on mechanical means such as the use of gimbals or hinges. The current state-of-the-art technologies demand more efficient methods for thrust vectoring, which minimize the use of mechanical components. These methods termed fluidic thrust vector control methods, employ secondary jets for achieving the required attitude, and trajectory of the aerospace vehicles such as aircraft, rockets, and missiles. Such methods have greatly helped in reducing vehicle weight, vehicle maintenance requirements, and enhancement of stealth characteristics of such vehicles. This work presents a review of the various fluidic thrust vectoring systems, starting with a brief overview of traditional thrust vectoring systems, followed by a discussion on the various aspects of fluidic thrust vectoring systems. It also highlights the effect of the various geometrical and operating conditions on the performance parameters of the thrust vectoring system such as the thrust vector angle, system thrust ratio, and thrust vectoring efficiency among others. For ensuring the comprehensive character of this work, synthetic jet vectoring techniques have also been included due to their nonmechanical nature and similarities with purely fluidic thrust vectoring techniques.
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      Fluidic Thrust Vector Control of Aerospace Vehicles: State-of-the-Art Review and Future Prospects

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    contributor authorDas, Arnab K.
    contributor authorAcharyya, Kaustubh
    contributor authorMankodi, Tapan K.
    contributor authorSaha, Ujjwal K.
    date accessioned2023-11-29T18:35:13Z
    date available2023-11-29T18:35:13Z
    date copyright4/3/2023 12:00:00 AM
    date issued4/3/2023 12:00:00 AM
    date issued2023-04-03
    identifier issn0098-2202
    identifier otherfe_145_08_080801.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4294240
    description abstractAn efficient propulsion system holds the key to the smooth operation of any aerospace vehicle over different flight regimes. Apart from generating the necessary thrust, emphasis has also been laid on vectoring the direction of thrust. The primitive modes of thrust vectoring chiefly focused on mechanical means such as the use of gimbals or hinges. The current state-of-the-art technologies demand more efficient methods for thrust vectoring, which minimize the use of mechanical components. These methods termed fluidic thrust vector control methods, employ secondary jets for achieving the required attitude, and trajectory of the aerospace vehicles such as aircraft, rockets, and missiles. Such methods have greatly helped in reducing vehicle weight, vehicle maintenance requirements, and enhancement of stealth characteristics of such vehicles. This work presents a review of the various fluidic thrust vectoring systems, starting with a brief overview of traditional thrust vectoring systems, followed by a discussion on the various aspects of fluidic thrust vectoring systems. It also highlights the effect of the various geometrical and operating conditions on the performance parameters of the thrust vectoring system such as the thrust vector angle, system thrust ratio, and thrust vectoring efficiency among others. For ensuring the comprehensive character of this work, synthetic jet vectoring techniques have also been included due to their nonmechanical nature and similarities with purely fluidic thrust vectoring techniques.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFluidic Thrust Vector Control of Aerospace Vehicles: State-of-the-Art Review and Future Prospects
    typeJournal Paper
    journal volume145
    journal issue8
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.4062109
    journal fristpage80801-1
    journal lastpage80801-29
    page29
    treeJournal of Fluids Engineering:;2023:;volume( 145 ):;issue: 008
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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