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Evaluation the Scramjet Cooling Heat for Available Work Using Exergy Analysis

Received: 13 July 2018     Accepted: 11 October 2018     Published: 12 November 2018
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Abstract

The scramjet cooling heat has a big potential work between the heat and the fuel coolant. However, there is no idea about the maximum potential work of the heat from cooling scramjet. Therefore, the potential work of the scramjet cooling heat is studied. The maximum available work from the heat of cooling scramjet is evaluated by the exergy analysis. The heat exergy analysis model is proposed under the heat sources condition according to the heat transfer performance of the scramjet wall and fuel coolant. It is supposed that a closed thermodynamic system is performed between hot source and cold source. The heat flow, the heat exergy and the available work from the scramjet wall are 543.1kW, 407.3kW and 370.3kW, respectively, when the temperature of scramjet wall is 1200K. And the exergy efficiency of the closed system is 68.2%. The exergy losses of external irreversible processes between the closed system and heat sources are analyzed by considering the heat exchanging temperature differences. The external exergy losses and the exergy efficiency have been largely changed with the heat exchanging temperature differences between the closed system and heat sources. The heat exchanging temperature differences are decreased, the external exergy losses are decreased and the exergy efficiency is increased. However, the heat exchanging temperature differences would be adapted to heat exchanging processes and decreasing the acreage of heat exchange. It is meaningful for having a guidance of power generation for hypersonic vehicle.

Published in International Journal of Energy and Power Engineering (Volume 7, Issue 4)
DOI 10.11648/j.ijepe.20180704.11
Page(s) 47-53
Creative Commons

This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.

Copyright

Copyright © The Author(s), 2018. Published by Science Publishing Group

Keywords

Scramjet, Exergy, Available Work, Exergy Loss

References
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  • APA Style

    Xinchun Li, Heyang Miao, Zhongwei Wang, Yaobin Niu. (2018). Evaluation the Scramjet Cooling Heat for Available Work Using Exergy Analysis. International Journal of Energy and Power Engineering, 7(4), 47-53. https://doi.org/10.11648/j.ijepe.20180704.11

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    ACS Style

    Xinchun Li; Heyang Miao; Zhongwei Wang; Yaobin Niu. Evaluation the Scramjet Cooling Heat for Available Work Using Exergy Analysis. Int. J. Energy Power Eng. 2018, 7(4), 47-53. doi: 10.11648/j.ijepe.20180704.11

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    AMA Style

    Xinchun Li, Heyang Miao, Zhongwei Wang, Yaobin Niu. Evaluation the Scramjet Cooling Heat for Available Work Using Exergy Analysis. Int J Energy Power Eng. 2018;7(4):47-53. doi: 10.11648/j.ijepe.20180704.11

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  • @article{10.11648/j.ijepe.20180704.11,
      author = {Xinchun Li and Heyang Miao and Zhongwei Wang and Yaobin Niu},
      title = {Evaluation the Scramjet Cooling Heat for Available Work Using Exergy Analysis},
      journal = {International Journal of Energy and Power Engineering},
      volume = {7},
      number = {4},
      pages = {47-53},
      doi = {10.11648/j.ijepe.20180704.11},
      url = {https://doi.org/10.11648/j.ijepe.20180704.11},
      eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ijepe.20180704.11},
      abstract = {The scramjet cooling heat has a big potential work between the heat and the fuel coolant. However, there is no idea about the maximum potential work of the heat from cooling scramjet. Therefore, the potential work of the scramjet cooling heat is studied. The maximum available work from the heat of cooling scramjet is evaluated by the exergy analysis. The heat exergy analysis model is proposed under the heat sources condition according to the heat transfer performance of the scramjet wall and fuel coolant. It is supposed that a closed thermodynamic system is performed between hot source and cold source. The heat flow, the heat exergy and the available work from the scramjet wall are 543.1kW, 407.3kW and 370.3kW, respectively, when the temperature of scramjet wall is 1200K. And the exergy efficiency of the closed system is 68.2%. The exergy losses of external irreversible processes between the closed system and heat sources are analyzed by considering the heat exchanging temperature differences. The external exergy losses and the exergy efficiency have been largely changed with the heat exchanging temperature differences between the closed system and heat sources. The heat exchanging temperature differences are decreased, the external exergy losses are decreased and the exergy efficiency is increased. However, the heat exchanging temperature differences would be adapted to heat exchanging processes and decreasing the acreage of heat exchange. It is meaningful for having a guidance of power generation for hypersonic vehicle.},
     year = {2018}
    }
    

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  • TY  - JOUR
    T1  - Evaluation the Scramjet Cooling Heat for Available Work Using Exergy Analysis
    AU  - Xinchun Li
    AU  - Heyang Miao
    AU  - Zhongwei Wang
    AU  - Yaobin Niu
    Y1  - 2018/11/12
    PY  - 2018
    N1  - https://doi.org/10.11648/j.ijepe.20180704.11
    DO  - 10.11648/j.ijepe.20180704.11
    T2  - International Journal of Energy and Power Engineering
    JF  - International Journal of Energy and Power Engineering
    JO  - International Journal of Energy and Power Engineering
    SP  - 47
    EP  - 53
    PB  - Science Publishing Group
    SN  - 2326-960X
    UR  - https://doi.org/10.11648/j.ijepe.20180704.11
    AB  - The scramjet cooling heat has a big potential work between the heat and the fuel coolant. However, there is no idea about the maximum potential work of the heat from cooling scramjet. Therefore, the potential work of the scramjet cooling heat is studied. The maximum available work from the heat of cooling scramjet is evaluated by the exergy analysis. The heat exergy analysis model is proposed under the heat sources condition according to the heat transfer performance of the scramjet wall and fuel coolant. It is supposed that a closed thermodynamic system is performed between hot source and cold source. The heat flow, the heat exergy and the available work from the scramjet wall are 543.1kW, 407.3kW and 370.3kW, respectively, when the temperature of scramjet wall is 1200K. And the exergy efficiency of the closed system is 68.2%. The exergy losses of external irreversible processes between the closed system and heat sources are analyzed by considering the heat exchanging temperature differences. The external exergy losses and the exergy efficiency have been largely changed with the heat exchanging temperature differences between the closed system and heat sources. The heat exchanging temperature differences are decreased, the external exergy losses are decreased and the exergy efficiency is increased. However, the heat exchanging temperature differences would be adapted to heat exchanging processes and decreasing the acreage of heat exchange. It is meaningful for having a guidance of power generation for hypersonic vehicle.
    VL  - 7
    IS  - 4
    ER  - 

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Author Information
  • Theoretical Training Department, the Air Force Xi’an Flight Academy, Xi’an, China

  • Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, China

  • Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, China

  • Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, China

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