This paper presents the design and development of a novel hypersonic flight vehicle capable of operating efficiently across subsonic, supersonic, and hypersonic speed regimes. The vehicle features a wedge-shaped aerofoil optimized for high-speed performance. Key aerodynamic parameters, including lift force, drag force, and velocity variation, are analyzed to assess the design efficiency. Computational flow analysis/CFD simulations are conducted using the finite volume method (FVM) with cuboidal mesh elements to accurately determine these parameters. The geometric modelling of the aircraft is done using Fusion 360 and OpenVSP, while the flow analysis is performed using ANSYS Fluent. The results showed a lift-to-drag ratio of 7.89 at subsonic speeds, 7.65 at supersonic speeds, and significant shockwave formations at hypersonic speeds, emphasizing the need for effective thermal protection systems. These findings provide significant inputs into the aerodynamic behaviour of hypersonic flight vehicles, contributing to the advancement of high-speed aerospace engineering. The results of this research provide significant inputs into the aerodynamic behaviour of hypersonic flight vehicles, contributing to the advancement of high-speed aerospace engineering.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Design and Computational Analysis of Hypersonic Flight Vehicle


    Weitere Titelangaben:

    Advances in Science, Technology & Innovation


    Beteiligte:
    Mukesh, R. (Herausgeber:in) / Venkata Ratnam, D. (Herausgeber:in) / Theerthamalai, P. (Herausgeber:in) / Lawrence Raj, Prince Raj (Herausgeber:in) / Tengli, P. N. (Autor:in) / Shetty, Tushar (Autor:in) / Aneyar, P. Ullas (Autor:in)

    Kongress:

    International Conference on Advances in Aerospace and Navigation Systems ; 2024 ; Bangalore, India August 22, 2024 - August 23, 2024



    Erscheinungsdatum :

    21.05.2025


    Format / Umfang :

    9 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Flight Control Design of Hypersonic Flight Experiment (HYFLEX) Vehicle

    Ishimoto, S. / Takizawa, M. / Suzuki, H. et al. | British Library Conference Proceedings | 1996


    Wing tip winglet folding mechanism of hypersonic flight vehicle and hypersonic flight vehicle

    GONG CHUNLIN / GOU JIANJUN / LI JINXING et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Thermal protection wall surface structure of hypersonic flight vehicle and hypersonic flight vehicle

    XU RUINA / JIANG PEIXUE / LIAO ZHIYUAN et al. | Europäisches Patentamt | 2024

    Freier Zugriff