Abstract This paper demonstrates that in transition from the one-dimensional longitudinal-channel motion of the coolant in the regenerative cooling system of the liquid propellant engine to the twodimensional (interchannel) channel motion (transpiration) through a porous mesh material (PMM), the hydraulic losses decrease. Experimental data on PMM hydraulic resistance coefficients and heat transfer in porous paths with the interchannel coolant transpiration (ICCT) is presented.


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    Titel :

    To Calculation of Regenerative Cooling of a Liquid Fuel Rocket Engine Chamber


    Beteiligte:
    Pelevin, F. V. (Autor:in) / Ponomarev, A. V. (Autor:in)

    Erschienen in:

    Russian Aeronautics ; 61 , 1 ; 71-77


    Erscheinungsdatum :

    2018-01-01


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    To Calculation of Regenerative Cooling of a Liquid Fuel Rocket Engine Chamber

    Pelevin, F. V. / Ponomarev, A. V. | Online Contents | 2018




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