This paper focus on the effects of Mach number on thermoelectric energy conversion for the limitation of aero-heating and the feasibility of energy harvesting on supersonic vehicles. A model of nose-tip structure constructed with SiC ceramics is developed to numerically study the thermoelectric performance in a supersonic flow field by employing the computational fluid dynamics and the thermal conduction theory. Results are given in the cases of different Mach numbers. Moreover, the thermoelectric performance in each case is predicted with and without Thomson heat, respectively. Due to the increase of Mach number, both the temperature difference and the conductive heat flux between the hot side and the cold side of nose tip are increased. This results in the growth of the thermoelectric power generated and the energy conversion efficiency. With respect to the Thomson effect, over 50% of total power generated converts to Thomson heat, which greatly reduces the thermoelectric power and efficiency. However, whether the Thomson effect is considered or not, with the Mach number increasing from 2.5 to 4.5, the thermoelectric performance can be effectively improved.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Effect of Mach number on thermoelectric performance of SiC ceramics nose-tip for supersonic vehicles


    Beteiligte:
    Han, Xiao-Yi (Autor:in) / Wang, Jun (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2014


    Format / Umfang :

    7 Seiten, 27 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch





    Synthesis of an airfoil at supersonic Mach number

    Schmit, Lucien A. / Thornton, William A. | TIBKAT | 1965


    Effect of Injection Mach Number on Penetration in a Supersonic Crossflow

    Li, Guang-Xin / Sun, Ming-Bo / Yu, Jiang-Fei et al. | AIAA | 2019



    Mach Number and Temperature Effects on Mach Wave Emission from Supersonic Jets

    Nonomura, T. / Fujii, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008